Zoom lens system

ABSTRACT

A zoom lens system is disclosed. The zoom lens system forms a final image of an object and a first intermediate real image between the object and the final image. The zoom lens system includes a first optical unit located between the object and the first intermediate real image. The first optical unit comprises at least one optical subunit which is moved to change the size (magnification) of the first intermediate real image. The zoom lens system also includes a second optical unit located between the first intermediate real image and the final image, at least a portion of which is moved to change the size (magnification) of the final image. The zoom lens system provides a wide zoom range of focal lengths with continuous zooming between the focal lengths.

CROSS-REFERENCE TO RELATED APPLICATION

This application is a Continuation-In-Part (CIP) application of U.S. patent application Ser. No. 10/622,914, filed Jul. 18, 2003, which claims the benefit of U.S. Provisional Application No. 60/397,882, filed Jul. 22, 2002, which application is specifically incorporated herein, in its entirety, by reference.

BACKGROUND OF THE INVENTION

1. Field of the Invention

This invention relates to optical lens systems for cameras and other optical devices, and, in particular, to high performance zoom lens systems that produce a high quality image over a full zoom range of focal lengths and are capable of being provided with an extremely large zoom ratio.

2. Description of Related Art

General Background of the Invention. The use of zoom lens systems for all types of photography, such as broadcast television, high definition television (“HDTV”), advanced television (“ATV”), video camcorders, film cinematography and still photography has become increasingly popular. As the use of zoom lens systems has increased, the demand for wider ranges of zooming capability, i.e. large zoom ratios, has also increased. For example, the zoom lens systems used in broadcast television have steadily increased in zoom ratio capability over the years to a maximum of about 101 to 1 at present but there is a demand for a still larger zoom ratio. While the focal length range of a conventional zoom lens system may be increased by the use of a drop-in extender or other multiplier, such as a broadcast television zoom lens system with a focal length range of 8.9 mm to 900 mm being increased to 17.8 mm to 1800 mm to increase the telephoto capability, this does not change the zoom ratio of about 101 to 1. Moreover, for broadcast television zoom lens systems there are somewhat different requirements for “studio” (indoor) or “outside broadcast” (outdoor) use concerning the focal length range and acceptable “f” numbers, whereby it has become conventional practice to employ two different zoom lens systems for indoor and outdoor broadcast television uses to maximize the capabilities for both types of uses.

Further, in addition to the demand and desirability of using zoom lens systems with wider ranges of focal lengths, such lenses must retain superior optical characteristics and performance that previously has been accomplished only by using separate objective lenses of different fixed focal lengths or zoom lens systems with a limited zoom ratio. As the zoom ratio increases, the difficulty in providing a high performance optical system with superior characteristics and performance also increases. Even most previously available zoom lens systems of a limited zoom range have one or more undesirable limitations such as the inability to focus adequately over the entire focal length range, the inability to focus on close objects, the lack of adequate optical performance over the entire focal length range and focus distance, the cost, the large size for the limited zoom range achieved and the like.

Still further, as the zoom range of a lens system increases, generally the length and weight increases whereby the difficulty in maintaining the lens and camera steady also increases. Therefore image stabilization also becomes an issue for the design of a practical zoom lens system having a large focal length range and zoom ratio.

Moreover, as the focal length range of a zoom lens system increases, generally the focusing problems also increase. Although close focusing at long focal lengths of the zoom range is not absolutely necessary, it is required at lesser focal lengths. In the past, continuous focusing over a considerable conjugate range from infinity to objects at a very short distance such as about 8 feet or less has been difficult to achieve. Further, the problem of “breathing” of the final image (where the perceived size changes as the focus distance is changed) at shorter focal lengths must be minimized to avoid, for example, one person disappearing from the scene as the focus is changed to another person at a different distance from the lens. These focus performance requirements, including maintaining the quality of the final image, tend to increase substantially the weight and cost of the zoom lens system unless the size can be minimized and performance maximized by the overall lens design, including glass selection.

Background Information Concerning Zooming. As discussed above, zoom lens systems with a wide-range of focal lengths are very desirable in numerous photographic applications, including broadcast television, cinematography and video and still photography. One standard zoom lens system used in these applications has a four-group PN(P or N)P structure, where P stands for a group of at least one lens element wherein the lens group has positive power, N stands for a group of at least one lens element wherein the lens group has negative power, and the groups are identified consecutively from the object space toward the image space, as is conventional. The front positive group is often called the focusing group because it can be moved for focusing the zoom lens system at any focal length position without the need to refocus for any other focal length of the zoom lens. The second negative group is the variator, and it induces significant magnification change during zooming. The third group, which can in general have either positive or negative power, is the compensator, and it is movable to insure that the image plane remains stationary. It also can provide some of the magnification change to effect zooming. The final positive fourth group is often called the prime lens group because it forms a sharp image.

This basic zoom lens system is suitable for zoom ratios of 50:1 or even more. As the zoom ratio is extended to about 100:1, however, the variator is required to change its object magnification to such an extent during zooming that aberrations become impracticably large and difficult to correct. In addition, at such large zoom ratios there is a very large change in entrance pupil location during zooming, and this tends to make the front group very large and difficult to correct. Another problem derives from the fact that, to reduce the aberration change that results from a large change of magnification, it is desirable that the variator have reduced optical powers. Weaker optical power, however, also increases the lens travel and length of the optical system. For a narrow field-of-view this would not be a problem, but, for a wide field-of-view, large motions lead to an increase in the principal ray heights at the rear portion of the lens system. Since the requirements for either the front or the rear of the lens system can be satisfied, but not simultaneously, this results in no ideal place for the aperture stop. If the stop is placed near the front of the lens, the front lens element diameters, and resultant aberrations, are reduced, and if the aperture stop is placed nearer to the rear part of the lens system, the rear lens diameters and resultant aberrations are decreased.

SUMMARY OF THE INVENTION

General Summary of the Invention. It is an object of the present invention to provide a zoom lens system that overcomes the problems and inefficiencies of prior zoom lens systems having large zoom ratios. A further object is to provide a zoom lens system with a wide zoom range of focal lengths and high performance characteristics for both indoor and outdoor use. A still further object of this invention is to provide a zoom lens system with a ratio of about 300 to 1 and a zoom range, for example, from about 7 mm to 2100 mm focal length, with continuous zooming between the focal lengths. Still another object of this invention is to provide a high performance zoom lens system with an optical system having a front zoom lens group for forming an intermediate image and a rear zoom lens group to magnify that image to thereby produce an extremely large zoom ratio. Still another object is to provide such a zoom lens system with optical image stabilization. Still another object is to provide such a zoom lens system with a focusing lens group capable of precise focusing over the entire focal length range of the zoom ratio.

Although of particular benefit for achieving large zoom ratios, the zoom lens systems of the invention can have conventional zoom ratios, e.g., zoom ratios associated with such consumer products as video camcorders, still cameras and the like. It is an additional object of the invention to produce zoom lens systems for these smaller zoom ratio applications.

Other and more detailed objects and advantages of the present invention will readily appear to those skilled in the art from the various preferred embodiments.

Summary of the Zoom Ratio Aspects of the Invention. The present invention overcomes the obstacles that currently limit zoom lens systems to a zoom ratio of about 101:1. The basic idea of the invention can be viewed as the use of a compound zoom lens system that consists of two separate zoom lens portions wherein the front zoom lens portion forms an intermediate image, and the rear zoom lens portion is a relay that transfers the intermediate image formed by the front zoom lens portion to the final image. The total zoom ratio of the complete compound zoom lens system is equal to the zoom ratio of the front zoom lens multiplied by the zoom ratio of the relay. Thus, if the zoom ratio of the front zoom lens portion is 20:1 and the zoom ratio of the relay is 15:1, then the zoom ratio of the entire compound zoom lens system is 300:1. The present invention can be used to achieve a zoom ratio of 300:1 or more, which greatly exceeds the practical limit of conventional zoom lens systems.

BRIEF DESCRIPTION OF THE DRAWINGS

FIGS. 1-5 are optical diagrams of compound zoom lens systems of the present invention for describing some of the principles and variations in the moving and fixed units employed in the system and some of the possible embodiments of the invention, with FIGS. 1-3 illustrating a system having about a 300:1 zoom ratio, FIGS. 4A and 4B having about a 130:1 zoom ratio and FIGS. 5A and 5B having about a 13:1 zoom ratio in an ultra wide angle lens system;

FIGS. 6A and 6B are optical diagrams of another embodiment of the zoom lens system of the present invention using three moving zoom lens groups, with the three zoom groups positioned for a short focal length in FIG. 6A and for a long focal length in FIG. 6B;

FIGS. 7A and 7B are optical diagrams of another embodiment of the zoom lens system of the present invention using four moving zoom lens groups, with the four zoom groups positioned for a short focal length in FIG. 7A and for a long focal length in FIG. 7B;

FIGS. 8A and 8B are optical diagrams of another embodiment of the zoom lens system of the present invention using four moving zoom lens groups, with the four zoom groups positioned for a short focal length in FIG. 8A and for a long focal length in FIG. 8B;

FIGS. 9A and 9B are optical diagrams of another embodiment of the zoom lens system of the present invention using three moving zoom lens groups, with the three zoom groups positioned for a short focal length in FIG. 9A and for a long focal length in FIG. 9B;

FIGS. 10-62 are figures that all relate to a single embodiment of the zoom lens system of the present invention that has a zoom ratio of about 300:1, with FIG. 10 being an optical diagram of the entire lens system, FIGS. 11-30 comprising optical diagrams of the lens system in 20 different representative positions of the movable lens elements, FIGS. 31-34 comprising optical diagrams of only the lens elements of the focus unit in four of the representative positions, FIGS. 35 and 36 illustrating only the front two zoom lens groups in two of the representative positions, FIGS. 37 and 38 illustrating only the rear zoom lens group in two of the representative positions, FIGS. 39-58 comprising ray aberration diagrams for the same 20 representative positions of all of the lens elements illustrated in FIGS. 11-30, respectively, FIG. 59 comprising a graph of the focus cam movement relative to the focus distances from minimum (bottom) to infinity (top), FIG. 60 comprising graphs of the three zoom cam movements relative to the system focal lengths, FIG. 61 comprising a graph of the “f” numbers of the system at the final image relative to the system focal lengths, and FIG. 62 comprising a graph of the stop diameters relative to the system focal lengths;

FIGS. 63 and 64 are an optical diagram and ray aberration graphs, respectively, for another embodiment of the zoom lens system of this invention incorporating a binary (diffractive) surface;

FIGS. 65 and 66 are an optical diagram and ray aberration graphs, respectively, for still another embodiment of the zoom lens system of this invention incorporating a binary (diffractive) surface; and FIGS. 67-70 are figures that relate to a still further embodiment of the invention having a zoom ratio of about 400:1 with FIGS. 67 and 68 being optical diagrams at focal lengths of 7.47 mm and 2983 mm, respectively, and FIGS. 69 and 70 being ray aberration graphs at focal lengths of 7.47 mm and 2983 mm, respectively;

FIGS. 71 and 72A-72D are optical diagrams for an example of still another embodiment of the zoom lens system of this invention incorporating a mirror for folding the lens for added compactness, with FIGS. 72A-72D showing the folded lens in a flat (unfolded) orientation for clarity, and illustrating various positions of the zoom groups;

FIGS. 73A-73C are optical diagrams for an example of an infrared (IR) embodiment of the zoom lens system of this invention, illustrating various positions of the zoom groups; and FIGS. 74-76 are ray aberration graphs corresponding to the position of the zoom groups shown in FIGS. 73A-73C, respectively;

FIG. 77 illustrates an unfolded layout of a second example of an IR embodiment of the zoom lens system of this invention, with lens elements and surfaces identified; FIGS. 78A-78F illustrate an unfolded layout of the second example IR embodiment at Zoom Positions Z1-Z6; and FIGS. 79A-79F illustrate the diffraction modulation transfer function (MTF) of selected light rays for the second example IR embodiment at the zoom positions shown in FIGS. 78A-78F.

DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS

In the following description of preferred embodiments, reference is made to the accompanying drawings, which form a part hereof, and in which is shown by way of illustration specific embodiments in which the invention may be practiced. It is to be understood that other embodiments may be utilized and structural changes may be made without departing from the scope of the preferred embodiments of the present invention.

In accordance with its general aspects, the invention provides a zoom lens system for forming a final image of an object, said system forming a first intermediate real image between the object and the final image, said system comprising:

-   -   (a) a first optical unit (e.g., lens elements 8 through 15 in         FIG. 10) located between the object and the first intermediate         real image, said unit comprising at least one optical subunit         which is moved to change the size (magnification) of the first         intermediate real image (e.g., lens elements 8 through 11 are         the primary source of magnification change for the first optical         unit in FIG. 10); and     -   (b) a second optical unit (e.g., lens elements 26 through 33 in         FIG. 10) located between the first intermediate real image and         the final image at least a portion of which (e.g., one or more         optical subunits or the entire second optical unit) is moved to         change the size (magnification) of the final image (e.g., in         FIG. 10, lens elements 26 through 28 of the second optical unit         are moved to change the size of the final image).

Preferably, the zoom lens system includes one or more optical subunits in either or both of the first and second optical units which is moved to hold the axial position of the final image substantially stationary as the focal length of the system is changed (e.g., lens elements 12 through 15 are the primary source of this function in FIG. 10). Such a subunit, however, may not be needed in all cases, e.g., if the overall optical system has an axially movable sensor.

Preferably, in addition to the first and second optical units, the zoom lens system comprises a focus unit (e.g., lens elements 1 through 7 in FIG. 10), a pupil imaging unit (e.g., lens elements 16 through 25 in FIG. 10), and/or an image stabilization unit (e.g., lens elements 34 through 39 in FIG. 10).

Preferably, the focus unit is (1) positioned in front of the first optical unit, (2) comprises two optical subunits that are movable along the zoom lens system's optical axis (e.g., lens element 2 and elements 3 and 4 in FIG. 10), and/or (3) comprises seven or less lens elements.

Preferably, the image stabilization unit comprises (1) at least one lens element that is laterally movable off the system's optical axis (e.g., lens elements 34 through 36 in FIG. 10), and/or (2) at least one lens element that is movable along the optical axis (e.g., lens elements 37 through 39 in FIG. 10). The light passing through the system is preferably substantially collimated between said laterally and axially movable lens elements of the image stabilization unit.

In addition to the first intermediate real image, the zoom lens systems of the invention can form additional intermediate real images between the object and the final image. The systems can include additional optical units besides the first and second units for changing the sizes (magnifications) of those additional intermediate real images.

Preferably, the first intermediate real image is formed in an air space between the optical elements of the zoom lens system (e.g., the lens elements, prisms, folding mirrors or the like used in the system) and does not pass through any surface of an optical element during zooming. When more than one intermediate real image is formed, this is also preferably true for all of the intermediate images.

The first optical unit in combination with other units of the system can have the form of a conventional zoom lens. Similarly, the second optical unit in combination with other units of the system can have a conventional zoom lens form. The overall system can thus be viewed as a “compounding” of two conventional zoom lenses with, in accordance with the invention, control of pupil imaging between the compounded zoom lenses.

The overall system can also be viewed as a front zoom lens which forms an intermediate image and a relay system which receives the intermediate image and changes its magnification to form the final image.

These approaches for describing the zoom lens systems of the invention are used herein in the detailed discussions of various aspects of the invention. Although these approaches provide a convenient way of describing the invention, it is to be understood that the invention is not limited to these descriptions and various embodiments and applications of the invention may not be completely amenable to such descriptions.

In accordance with other aspects, the invention provides a zoom lens system for forming a final image of an object, said system having a range of focal lengths between a maximum focal length and a minimum focal length and forming at least a first intermediate real image between the object and the final image for all focal lengths within said range, said system comprising:

-   -   (a) a first lens unit having a focal length that is changed to         change the size (magnification) of the first intermediate real         image, said first lens unit being located between the object and         the first intermediate real image for all focal lengths within         said range; and     -   (b) a second lens unit for changing the size (magnification) of         the final image, said second lens unit being located between the         first intermediate real image and the final image for all focal         lengths within said range.

In accordance with additional aspects, the invention provides a zoom lens system which comprises a variable focal length front lens unit which forms an intermediate real image and a variable magnification rear lens unit which forms an image (preferably, a real image) of the intermediate image.

In accordance with further aspects, the invention provides a compound zoom lens system that collects radiation from an object space and delivers the radiation to a final image in image space, said system comprising multiple zoom lens portions including a first zoom lens portion forming an intermediate image of the radiation from the object space and a last zoom lens portion forming the final image in the image space.

In accordance with still further aspects, the invention provides a zoom lens system for forming a final image of an object, said system having an optical axis, a front lens surface, an aperture stop, and a chief ray which crosses the optical axis at the aperture stop, said system comprising first and second lens units that are moved to change the focal length of the system, wherein:

-   -   (a) between the front lens surface and the final image, the         chief ray crosses the optical axis at at least one other         location besides said aperture stop for all focal lengths of the         system; and     -   (b) the system forms an intermediate real image that is located         between the first and second lens units for all focal lengths of         the system.

Description of Some Zooming Principles and Systems of the Invention. There are some unique aspects to a compound zoom lens system (i.e., a front zoom/zoom relay system) that enables an extraordinarily high degree of optical correction to be achieved. Imagine for a moment a simplified scenario in which the complete zooming motion takes place in stages. In the first stage the relay is initially set at a short focal length position that provides a small magnification of the intermediate image. The object conjugate of the relay will then have a small numerical aperture NA and its image conjugate will have a large numerical aperture NA. (As conventionally defined, the numerical aperture “NA” is equal to the sine of the vertex angle of the largest cone of meridional rays that can enter or leave an optical system or element, multiplied by the refractive index of the medium in which the vertex of the cone is located; and in the lens system optical prescriptions set forth below the “f” number equals the inverse of twice NA, i.e. f=1/2×NA). Since the NA in object space for the relay is equal to the NA in image space for the front zoom lens portion, then it is clear that in this first stage, the front zoom lens portion need only be well corrected for a small NA.

In the second stage, the front zoom lens portion is stationary at its long focal length position, and the relay then zooms to magnify the intermediate image to a greater and greater extent. As the focal length of the system increases during this second stage, the image NA of the relay becomes smaller and the object NA of the relay becomes larger. Hence, the image NA of the front zoom lens portion must also become larger. However, at the same time, the radial part of the intermediate image that is actually used becomes smaller and smaller as the system focal length gets larger.

Thus, the front zoom lens portion need not be corrected for a simultaneously large intermediate image size and a large relative aperture (NA). Rather, it needs to be corrected for a large intermediate image size at a small aperture, and for a small intermediate image size at a large aperture. This makes the design of the front zoom lens portion considerably easier than the design of a traditional zoom lens system having the same zoom ratio as the front zoom lens system of the present invention.

Likewise, the relay need only be corrected for a large image NA and large object size at the small magnification end of its focal lengths. At the other end of its zoom range of focal lengths, the object size is small and the image NA is also small.

As discussed above, in addition to a front zoom lens portion and a relay, the zoom lens systems of the invention preferably also include a pupil imaging unit. This unit serves to image the exit pupil of the front zoom lens portion into the entrance pupil of the relay. By selecting the appropriate powers, not only can the lens diameters, and attendant aberrations, of the relay be minimized, but control of the exit pupil position of the system can be improved.

As also discussed above, the intermediate image formed by the front zoom lens portion is preferably located at a position where it does not pass through any lens surfaces as the system is zoomed from its minimum to its maximum focal lengths. By being between the front zoom lens portion and the rear relay, the intermediate image is automatically behind the axially moving lens unit or units that provide zooming in the front zoom lens portion and in front of any axially moving lens units that provide zooming in the rear zoom portion. Since in certain embodiments of the invention the intermediate image can move during zooming, the locations for the lens surfaces on either side of the intermediate image, whether those surfaces are fixed or moving, are preferably chosen so that notwithstanding the motion of the intermediate image, the surfaces remain spaced from the intermediate image throughout the zoom range of the system.

Various of the foregoing features of the invention are illustrated in FIGS. 1-3 for a PNPP-PNPP compound zoom lens system with a zoom ratio of about 300:1. As indicated in FIG. 1, this compound zoom lens system has a front zoom lens portion with a zoom ratio of about 20:1 and a rear zoom lens portion (relay) with a zoom ratio of about 15:1. The groups and their positive or negative power signs are also indicated in FIG. 1. In this compound zoom lens system, the relay is stationary as the front zoom lens portion is operated from its shortest focal length position (shown in FIG. 1) to its longest focal length position (shown in FIG. 2). Once the front zoom lens portion reaches its long focal length position, the relay begins to vary the magnification of the intermediate image to further increase the focal length of the compound system. FIG. 3 shows the system in its maximum focal length condition, in which the front zoom lens portion is at its maximum focal length position and the rear zoom (relay) lens portion is in its maximum magnification position.

FIGS. 1 and 2 show the small NA at the intermediate image plane and large NA at the final image plane that occurs during the initial phase of zooming from short to long. The size of the intermediate image is large during this phase, as shown in the figures. FIG. 3 shows that the NA becomes larger at the intermediate image and smaller at the final image at the longest focal length position.

Note that in this example there are 8 zoom lens groups, but only 4 of them are independently movable for zooming. The 1st, 4th, 5th, and 8th groups are all stationary with respect to the final image. During focusing, however, one or more of these groups can be made to move.

The scenario sketched out here is for exemplary purposes. In practice, the zooming motion need not be clearly divided into two stages, and as a result the relay or a part of it can move during the initial zooming stages and not just near the long end of the focal lengths.

The example of FIGS. 1-3 described above has a PNPP-PNPP construction in which the dash “-” signifies the end of the front zoom lens portion. Both the front zoom lens portion and rear zoom lens portion have variator and compensator zooming groups. One advantage of this configuration is that the intermediate image can be made absolutely stationary if desired. Rendering the image stationary will prevent it from passing through any optical surface that might reveal surface flaws and dust images that will appear at the final image. Using a four-group construction in the rear zoom lens portion also permits better control of the exit pupil position, which may be important for matching the telecentricity requirements of certain image sensors.

If movement of the intermediate image can be tolerated, then it is possible to eliminate one of the compensators. Removal of the rear compensator is preferred in this case because it only moves when the beam diameters are relatively small. The resulting construction will then be a PNPP-PNP configuration.

For both of these configurations care must be taken to match the exit pupil of the front zoom lens portion with the entrance pupil of the relay. For this purpose, an eyepiece-like group is beneficial for converting the diverging beams emanating from the intermediate image into approximately parallel beams entering a normal PNP- or PNPP- type zoom lens system corrected for infinite conjugates.

One aspect of high-speed (large aperture) ultra-wide-range of focal lengths compound zoom lens systems of this type is that the intermediate image and all of its image faults are highly magnified by the zoom groups in the relay at the long focal length position. This places stringent requirements on the correction of secondary color aberrations in the front zoom lens portion and especially the focusing group. In order to accomplish this correction, it is necessary to use at least one, and more likely several, fluor-crown glass elements. As an alternative, calcium fluoride or binary (diffractive) surfaces could also be used for this purpose.

A variety of binary (diffractive) surfaces (diffractive elements) can be used in the practice of the invention. For example, for certain applications, one or more diffractive optical elements of the type disclosed in U.S. Pat. No. 6,507,437, assigned to Canon, can be used, either alone or in combination with other approaches for correcting chromatic aberrations.

One big advantage of using a PNPP-PNPP or PNPP-PNP configuration over existing zoom lens systems is that both the front zoom lens portion and the rear zoom lens portion (relay) system can have very large zoom ratios. It is quite reasonable to have a zoom ratio of 20:1 or more for either the front zoom lens portion or the rear zoom lens portion in this case, so that a total zoom ratio of 400:1 or more is possible. However, if such a large zoom ratio is not required, it is possible to simplify the system significantly by instead using a relay with an NP configuration having two moving groups. Such a relay is very useful for large aperture applications with a total zoom ratio in the relay of about 3:1 to about 10:1. An example of a compound zoom lens system with a zoom ratio of about 130:1 having an about 20:1 zoom ratio PNPP front zoom lens portion and an about 6.5:1 zoom ratio relay is shown in FIGS. 4A and 4B. FIG. 4A illustrates the minimum focal length of about 7 mm and FIG. 4B illustrates the maximum focal length of about 900 mm. One disadvantage of this configuration is that the rearmost lens group is not stationary; hence it must be designed to withstand a considerable change of magnification at large apertures, which makes it somewhat difficult to design.

An even further simplified construction consisting of an NP front zoom lens portion and an NP rear zoom lens portion (relay) can also be designed, although the maximum zoom ratio in this case will be lowered. Clearly, the technique can be generalized to include a large number of combinations of various zoom lens arrangements for the front zoom lens portion and for the rear zoom lens portion. For example, a high zoom ratio, ultra wide angle zoom lens system can be constructed by using an NP, NPP or NPNP ultra wide angle front zoom lens portion having a zoom ratio of about 2:1 with an NP rear zoom lens portion (relay) having a zoom ratio of about 6.5:1. The result would be a compound zoom lens system with a zoom ratio of about 13:1 with a maximum full field of view of up to 100 degrees or more. FIGS. 5A and 5B illustrate a 4.4 mm-57.2 mm, f/3-f/7 compound zoom lens system with a zoom ratio of about 13:1 for a ⅔″ sensor. The full-field angle at the wide-angle end of this compound zoom lens system is more than 102 degrees. Clearly, a PNPP-type rear zoom lens portion (relay) similar to the one used in FIGS. 1-3 could be used with this same ultra wide angle front zoom lens portion to yield an ultra wide angle compound zoom lens system with a zoom ratio of about 30:1.

The existence of an intermediate image is common to all of these configurations, and this offers some unique opportunities for aberration correction that are not typically available in zoom lens system types of the prior art. For example, aspheric surfaces placed on elements located near the intermediate image can have a strong impact on distortion and other field aberrations without disturbing the spherical aberration correction. Advantages of placing an aspheric surface in this area include that the tolerances are generous because the beam diameters are small, and the elements themselves are small. This means that the cost of using aspheric surfaces in this region is minimal.

Detailed Description of the Preferred Embodiments. As described above in the section entitled “Description of Some Zooming Principles and Systems of the Invention”, each of the herein disclosed embodiments of the present invention includes a front zoom lens portion and a rear zoom lens portion thereby forming a compound zoom lens system. An intermediate image is formed after the front zoom lens portion whereby the rear zoom lens portion functions as a zoom relay to magnify the intermediate image so as to produce the magnified final image for capturing by film or any other kind of light detector or capture device, such as a charge coupled device (CCD), in a camera. For purposes of this application, the term “camera” is used generically to describe any kind of light detecting or capturing device that may be placed after the lens system of the present invention, including a still, video or movie capture device, whether containing film, videotape, optical disk, CMOS, CCD or another storage medium, or an eyepiece or the human eye. Any such “camera” may include additional lens elements. At present it is contemplated that the front zoom lens portion will be comprised of two moving zoom lens groups and the rear zoom lens portion will be comprised of either one or two moving zoom lens groups, but it is to be understood that more or fewer moving zoom lens groups may be used without departing from the present invention. Also, at present it is contemplated that only one intermediate image will be formed in the entire compound zoom lens system but other embodiments of the present invention may form more than one intermediate image.

In addition to the front and rear zoom lens portions, the compound zoom lens system of the present invention preferably includes a focus lens group. It is preferred that the focus lens group be positioned at the front of the lens system, as shown by each of the embodiments disclosed herein, although it is possible to accomplish some and maybe all of the focusing elsewhere in the compound zoom lens system in other embodiments of the invention.

When a single intermediate image is formed in this compound zoom lens system, the final image is upside down and reversed left-to-right from the conventional orientation produced by an objective lens and therefore the image orientation must be accommodated by the camera. For a video camera using a single chip for the detector, it is possible to merely rotate the chip 180 degrees about the optical axis so that the chip reads the final image as though it is conventionally oriented. Another solution to the orientation problem for a video camera is to reverse the order in which the data is scanned, i.e. instead of from left-to-right and top-to-bottom the data can be read right-to-left and bottom-to-top to achieve the conventional orientation. Still another solution to the orientation problem for a video camera that uses a “frame store” feature to store an entire frame on a memory chip before it is transmitted for use is to merely transmit the stored frame from the frame store memory in the reverse order. For a movie film camera, the entire camera with the film magazine may be turned upside down to, as a result, run the film upwardly for correcting the image orientation. Another solution for the orientation of the image in a movie film camera used in the conventional manner and employing the present zoom lens system is to use digital compositing wherein the film is digitally scanned and then, for example, after digital manipulation the image is imposed on new film in the conventional orientation. The use of a prism in or in connection with the lens system of this invention will also correct the orientation of the final image. For this approach, care must be taken so that the prism will not cause excessive deterioration of the quality of the final image, especially for high performance applications of the present lens system.

Due to the compound zoom arrangement of the zoom lens system of the present invention, the body of the compound lens system will often be of substantial length and therefore any deflection or vibration of the lens system relative to the camera may cause unacceptable deflection or vibration of the final image in the camera. Thus, at least for compound zoom lens systems of the present invention having large zoom ratios, long focal lengths and/or substantial length, it is contemplated that an image stabilization arrangement will be employed. While electronic image stabilization may be appropriate for some video camera applications, for higher performance zoom lens system applications it is preferred that an optical image stabilization arrangement be included in the body of the compound zoom lens system and preferably near the camera end of the lens system, such as is included in the embodiment of FIGS. 10-62 described below.

Although it is more desirable to design and construct the compound zoom lens system of this invention as an integral unit for maximum performance, it is also possible to use two or more separable components to achieve the basic features. For example, a conventional zoom lens or a modified form thereof may be used as the front zoom lens portion and then the rear zoom lens portion may be comprised of a separate attachment that relays and varies the magnification of (e.g. zooms) the image formed by the front zoom lens portion, which image becomes the “intermediate” image, to form the final image. Thus, the front zoom lens portion will provide one zoom ratio and the rear attachment zoom portion will provide another zoom ratio. However, for such a combination, the pupil imaging should be controlled to obtain a final image of acceptable optical quality. Other such combinations of conventional and/or modified lens portions may also be used to provide the compound zoom lens system of the present invention.

FIGS. 6A through 9B illustrate optical diagrams for four different embodiments of the zoom lens system of the present invention. At the far right of each of the FIGS. 6A-9B the two rectangular blocks represent the prism blocks for a conventional 3 CCD ⅔″ detector, which is part of the video camera and therefore not part of the zoom lens system.

The following tables list the lens system optical prescriptions, the variable thickness positions for various surfaces, and the focal lengths and magnifications for various surface groups for each of those four embodiments. For simplicity and clarity in view of the large number of surfaces and the small scale of the optical diagrams that include all of the elements, only some of the surfaces in FIGS. 6A through 9B that correspond to the surfaces set forth in the lens system optical prescriptions are identified. A more detailed explanation of the tables is provided following the tables. TABLES FOR FIGS. 6A & 6B LENS SYSTEM OPTICAL PRESCRIPTION Glass Glass Surface Radius Thickness Index Dispersion OBJECT Infinity Infinity S1 925.010 10.000 1.90135 31.5 S2 280.601 20.595 S3 626.503 19.748 1.49699 81.6 S4 −2050.828 0.300 S5 −2871.294 12.027 1.49699 81.6 S6 −624.468 0.300 S7 266.779 14.079 1.49699 81.6 S8 497.283 0.300 S9 351.230 16.228 1.49699 81.6 S10 1246.212. 0.300 S11* 185.443 25.083 1.49699 81.6 S12 839.856 Variable S13 301.162 5.346 1.77249 49.6 S14* 71.693 15.360 S15 −3690.461 2.000 1.77249 49.6 S16 100.162 27.480 S17 −70.544 5.456 1.80400 46.6 S18 −3458.086 8.858 1.92286 18.9 S19 −125.683 Variable S20 −257.845 12.063 1.49699 81.6 S21 −78.411 0.127 S22 149.706 13.001 1.49699 81.6 S23 −98.095 2.000 1.80349 30.4 S24 −266.962 0.100 S25 114.669 6.712 1.49699 81.6 S26 485.498 Variable STOP Infinity 24.165 S28* −41.960 2.000 1.60311 60.7 S29 40.078 31.156 1.69894 30.1 S30 83.406 12.225 S31 −64.844 2.590 1.60311 60.7 S32 912.611 13.001 1.69894 30.1 S33 −52.224 24.076 S34 99.845 2.313 1.49699 81.6 S35 167.386 15.000 S36 155.608 14.122 1.49699 81.6 S37 −47.886 9.568 1.87399 35.3 S38 −67.571 0.018 S39 381.504 2.000 1.87399 35.3 S40 49.653 11.590 1.43875 95.0 S41 −583.112 43.970 S42* 50.132 14.235 1.43875 95.0 S43 482.784 Variable S44 −23.147 2.000 1.69100 54.8 S45* 32.021 1.889 S46 52.655 21.412 1.84666 23.8 S47 −380.467 Variable S48 102.416 11.302 1.49699 81.6 S49 −50.958 0.405 S50* 34.098 13.134 1.49699 81.6 S51 43.222 1.521 S52 58.738 10.784 1.49699 81.6 S53 −35.052 2.000 1.74319 49.3 S54 43.422 1.334 S55 57.389 10.079 1.49699 81.6 S56 −38.685 0.658 S57 −35.272 3.772 1.78472 25.7 S58 −56.940 0.500 S59 166.529 4.833 1.69100 54.8 S60 −100.192 0.250 S61 83.273 5.608 1.69100 54.8 S62 808.1 Variable S63 Infinity 13.200 1.51680 64.1 S64 Infinity 2.000 S65 Infinity 33.000 1.60859 46.4 S66 Infinity 5.000 IMAGE Infinity Note: Maximum image diameter = 11.0 mm *Surface profiles of asphenc surfaces S11, S14, S28, S42, S45 and S50 are governed by the following conventional equation: $Z = {\frac{({CURV})Y^{2}}{1 + \left( {1 - {\left( {1 + K} \right)({CURV})^{2}Y^{2}}} \right)^{1/2}} + {(A)Y^{4}} + {B(Y)}^{6} + {(C)Y^{8}} + {(D)Y^{10}}}$ where: CURV = 1/(Radius of Surface) Y = Aperture height, measured perpendicular to optical axis K, A, B, C, D = Coefficients Z = Position of surface profile for a given Y value, as measured along the optical axis from the pole (i.e. axial vertex) of the surface. The coefficients for The coefficients for the surface S11 are: the surface S42 are: K = −0.2197954 K = −0.0460624 A = 9.0593667e−009 A = −2.6257869e−007 B = 1.7844857e−013 B = −2.5945471e−010 C = 1.5060271e−017 C = 2.4316558e−013 D = −9.7397917e−023 D = −1.2995378e−016 The coefficients for The coefficients for the surface S14 are: the surface S45 are: K = 0.7048333 K = 0.0 A = −3.0463508e−007 A = −1.1056187e−005 B = −1.1451797e−010 B = 2.8606310e−008 C = 3.4844023e−014 C = −1.2655154e−010 D = −2.2107339e−017 D = 2.2826095e−013 The coefficients for The coefficients for the surface S28 are: the surface S50 are: K = −0.9252575 K = 0.0 A = −1.8743376e−007 A = −1.8976230e−006 B = −1.0562170e−009 B = 1.2489903e−009 C = 2.8892387e−012 C = −2.3703340e−012 D = −3.6671423e−015 D = 3.0161146e−015 VARIABLE THICKNESS POSITIONS AND DATA P1 P2 P3 P4 P5 P6 P7 P8 EFL 7.257 9.008 16.013 36.022 82.023 174.970 399.652 900.099 F/No. 1.450 1.450 1.450 1.450 1.450 2.000 4.000 5.000 S12 1.000 23.202 72.004 118.539 150.121 162.578 162.380 162.474 S19 243.711 218.457 160.764 96.265 43.111 0.500 57.093 0.500 S26 1.000 4.080 12.979 30.924 52.631 82.760 26.357 82.523 S43 142.978 142.908 142.764 142.760 142.409 140.110 89.130 81.860 S47 8.255 8.273 8.377 8.434 8.540 4.765 3.198 5.165 S62 19.000 19.000 19.000 19.000 19.000 25.160 77.703 83.508 Surface Groups Focal Lengths S1-S12 266.611 S13-S19 −46.300 S20-S26 91.566 S27-S43 55.841 S44-S47 −32.720 S48-S62 42.594 Surface Group Magnifications Surfaces P1 M′ P1 MP′ P2 M′ P2 MP′ P3 M′ P3 MP′ P4 M′ P4 MP′ S1-S12 0.000 0.754 0.000 0.672 0.000 0.492 0.000 0.320 S13-S19 −0.238 7.670 −0.268 7.215 −0.374 6.275 −0.599 5.828 S20-S26 −0.350 0.876 −0.385 0.843 −0.495 0.746 −0.699 0.550 S27-S43 0.871 −1.159 0.870 −1.159 0.854 −1.159 0.844 −1.159 S44-S47 0.321 −2.846 0.322 −2.829 0.325 −2.794 0.327 −2.793 S48-S62 −1.170 −0.304 −1.170 −0.305 −1.170 −0.308 −1.170 −0.308 Surfaces P1 M′ P5 MP′ P6 M′ P6 MP′ P7 M′ P7 MP′ P8 M′ P8 MP′ S1-S12 0.000 0.195 0.000 0.123 0.000 0.163 0.000 0.124 S13-S19 −1.012 7.410 −1.390 −119.200 −1.382 4.682 −1.386 −141.400 S20-S26 −0.945 −0.312 −1.275 −0.017 −0.715 0.599 −1.279 −0.014 S27-S43 0.834 −1.159 0.833 −1.159 0.774 −1.159 0.826 −1.159 S44-S47 0.330 −2.712 0.338 −2.278 0.769 −0.501 0.856 −0.451 S48-S62 −1.170 −0.313 −1.315 −0.361 −2.549 −0.731 −2.693 −0.727 Where, P1 M′ is lens group magnification of lens group which equals (entrance marginal ray angle)/exit marginal ray angle) and, P1 MP′ is lens group magnification which equals entrance principal ray angle/exit pnndpal ray angle and so on, up to P8 M′ and P8 MP′; the first two characters representing position number, for example P1 M′ and P1 MP′ are for position 1.

TABLES FOR FIGS. 7A & 7B LENS SYSTEM OPTICAL PRESCRIPTION Glass Glass Surface Radius Thickness Index Dispersion OBJECT Infinity Infinity S1 1273.174 10.255 1.80099 35.0 S2 475.265 1.538 S3 510.054 10.255 1.80099 35.0 54 279.310 14.066 S5 459.720 19.331 1.49699 81.6 S6 21434.630 0.308 S7 800.941 10.451 1.49699 81.6 S8 27454.520 0.308 S9 309.779 13.334 1.49699 81.6 S10 634.103 0.308 S11 361.606 17.818 1.49699 81.6 S12 2023.306 0.308 S13* 172.930 25.353 1.49699 81.6 S14 568.502 Variable S15 330.425 2.070 1.77249 49.6 S16* 73.838 18.829 S17 726.741 2.051 1.77249 49.6 S18 102.189 25.577 S19* −73.683 6.352 1.77249 49.6 S20* 359.798 9.948 1.80809 22.8 S21 −116.821 Variable S22 −176.211 5.797 1.49699 81.6 S23 −69.609 0.003 S24 144.415 20.317 1.49699 81.6 S25 −85.878 2.051 1.80349 30.4 S26 −282.651 0.000 S27 85.718 6.142 1.49699 81.6 S28 157.754 Variable STOP Infinity 22.498 S30* −34.201 2.051 1.60729 59.4 S31 42.409 2.743 1.69894 30.1 S32 101.162 4.085 S33 −82.300 3.589 1.60311 60.7 S34 −90.892 3.444 1.69894 30.1 S35 −39.457 6.472 S36 51.200 7.178 1.49699 81.6 S37 55.671 15.382 S38 67.S46 6.750 1.49699 81.6 S39 −47.804 3.076 1.87399 35.3 S40 −74.620 0.018 S41 95.357 3.076 1.87399 35.3 S42 35.060 30.000 1.43875 95.0 S43 −130.232 68.459 S44 Infinity 2.051 S45 Infinity 2.051 1.77249 49.6 S46 −341.189 8.763 S47* −30.765 4.102 1.78469 26.3 S48 −36.525 21.109 1.51680 64.2 S49 −30.389 0.308 S50 −160.796 14.522 1.51680 64.2 S51 −66.413 0.308 S52 461.095 8.390 1.51680 64.2 S53 −109.832 7.208 S54* 247.113 3.076 1.84666 23.8 S55 57.348 10.868 1.49699 81.6 S56 −56.360 0.289 S57 −73.106 5.307 1.63853 55.4 S58 −44.690 Variable S59 −28.736 3.076 1.83400 37.2 S60 115.838 2.771 S61 −31.347 2.871 1.83480 42.7 S62 −73.220 2.468 S63 −57.858 7.254 1.84665 23.9 S64 −24.994 0.005 S65 −29.067 2.871 1.80400 46.6 S66 −49.737 Variable S67 507.291 2.051 1.74319 49.3 S68 104.703 7.178 1.49699 81.6 S69 −76.662 Variable S70* 69.871 8.624 1.49699 81.6 S71 −663.734 8.908 S72 −155.686 3.076 1.84665 23.9 S73 −1137.705 0.202 S74 54.109 8.050 1.49699 81.6 S75 −73.493 0.393 S76 −66.184 2.871 1.74319 49.3 577 −99.535 19.484 578 Infinity 13.537 1.51633 64.1 579 Infinity 2.051 580 Infinity 33.841 1.60859 46.4 581 Infinity 5.019 IMAGE Infinity Note: Maximum image diameter = 11.0 mm *Surface profiles of aspheric surfaces S13, S16, S19, S20, S30, S47, S54 and S70 are governed by the following conventional equation: $\begin{matrix} {Z = {\frac{({CURV})Y^{2}}{1 + \left( {1 - {\left( {1 + K} \right)({CURV})^{2}Y^{2}}} \right)^{1/2}} + {(A)Y^{4}} + {B(Y)}^{6} + {(C)Y^{8}} + {(D)Y^{10}} +}} \\ {{(E)Y^{12}} + {(F)Y^{14}} + {(G)Y^{16}}} \end{matrix}\quad$ where: CURV = 1/(Radius of Surface) Y = Aperture height, measured perpendicular to optical axis K, A, B, C, D, E, F, G = Coefficients Z = Position of surface profile for a given Y value, as measured along the optical axis from the pole (i.e. axial vertex) of the surface. The coefficients for the The coefficients for the The coefficients for the surface S13 are: surface S20 are: surface S54 are: K = −0.1600976 K = 0.0 K = 0.0 A = 6.9210418e−009 A = 3.4619978e−008 A = −2.743254e−006 B = 2.2313210e−013 B = 4.2692157e−011 B = −2.133804e−009 C = 1.1852054e−017 C = −7.0823340e−014 C = 1.668568e−011 D = −2.0918949e−021 D = −2.3957687e−017 D = −1.9544629e014 E = 2.2579263e−025 E = 5.4513203e−020 E = 0.0 F = 8.1799420e−030 F = −1.4597367e−023 F = 0.0 G = −1.2582071e−033 G = −4.1263059e−027 G = 0.0 The coefficients for the The coefficients for the The coefficients for the surface S16 are: surface S30 are: surface S70 are: K = 0.9059289 K = −0.8025959 K = −2.3 A = −4.3564263e−007 A = −3.8556154e−007 A = 3.877213e−007 B = −1.3760665e−010 B = −5.4410316e−010 B = 4.916800e−010 C = 1.1349273e−014 C = 7.0427510e−012 C = −1.461192e−012 D = −3.8588303e−017 D = −8.5740313e−015 D = −3.258352e−017 E = 1.5211558e−020 E = −5.2635786e−017 E = 4.664784e−018 F = −5.1726796e−025 F = 1.0608042e−019 F = −4.216175e−021 G = −2.0900671e−027 G = 7.5783088e−023 G = 0.0 The coefficients for the The coefficients for the surface S19 are: surface S47 are: K = 0.0 K = 0.0 A = −6.5866466e−008 A = −1.2184510e−005 B = −3.2305127e−011 B = 1.2115245e−007 C = −3.5095033e−014 C = −3.0828524e−010 D = 4.0315700e−017 D = −5.7252449e−014 E = −6.1913043e−021 E = 0.0 F = −2.4403843e−023 F = 0.0 G = 9.0865109e−027 G = 0.0 VARIABLE THICKNESS POSITIONS AND DATA P1 P2 P3 P4 P5 P6 P7 EFL 7.257 12.152 35.981 82.040 145.068 736.934 2088.142 F/No. 1.450 1.450 1.450 1.450 1.450 7.200 12.500 S14 1.026 51.867 122.026 160.824 167.824 157.900 167.823 S21 262.564 202.199 103.948 49.493 0.000 34.351 0.000 S28 1.563 11.088 39.178 55.576 97.329 72.903 97.329 S58 8.616 8.616 8.616 8.616 8.616 99.467 105.316 S66 111.358 111.358 111.358 111.358 111.358 53.699 0.000 S69 38.387 38.387 38.387 38.387 38.387 5.195 53.100 Surface Groups Focal Lengths  S1-S14 283.564 S15-S21 −52.598 S22-S28 102.619 S29-S58 51.668 S59-S66 −29.319 S67-S69 178.034 S70-S77 70.650 Surface Group Magnifications Surfaces P1 M′ P1 MP′ P2 M′ P2 MP′ P3 M′ P3 MP′ P4 M′ P4 MP′ S1-S14 0.000 0.740 0.000 0.564 0.000 0.318 0.000 0.179 S15-S21 −0.260 7.365 −0.347 6.511 −0.644 6.193 −1.207 7.342 S22-S28 −0.369 0.833 −0.462 0.740 −0.736 0.466 −0.896 0.306 S29-S58 −2.392 −0.356 −2.392 −0.356 −2.392 −0.356 −2.392 −0.356 S59-S66 −0.282 25.995 −0.282 25.995 −0.282 25.993 −0.282 25.994 S67-S69 14680.000 0.231 14680.000 0.231 14680.000 0.231 14680.000 0.231 S70-S77 0.000 0.447 0.000 0.447 0.000 0.447 0.000 0.447 Surfaces PS M′ P5 MP′ P6 M′ P6 MP′ P7 M′ P7 MP′ S1-S14 0.000 0.117 0.000 0.174 0.000 0.117 S15-S21 −1.468 −19.350 −1.150 14.886 −1.468 −19.350 S22-S28 −1.303 −0.101 −1.065 0.137 −1.303 −0.101 S29-S58 −2.392 −0.356 −2.392 −0.356 −2.392 −0.356 SS9-S66 −0.282 25.994 −2.227 0.319 −4.006 0.300 S67-S69 14680.000 0.231 271.410 2.365 81.569 1.386 S70-S77 0.000 0.447 −0.001 −0.374 −0.005 −1.131 Where, P1 M′ is lens group magnification of lens group which equals (entrance marginal ray angle)/(exit marginal ray angle) and, P1 MP′ is lens group magnification which equals entrance principal ray angle/exit principal ray angle and so on, up to P7 M′ and P7 MP′; the first two characters representing position number, for example P1 M′ and P1 MP′ are for position 1.

TABLES FOR FIGS. 8A & 8B LENS SYSTEM OPTICAL PRESCRIPTION Glass Glass Surface Radius Thickness Index Dispersion OBJECT Infinity Infinity S1 −763.589 10.000 1.80099 35.0 S2 408.783 15.991 S3 1218.452 22.500 1.49699 81.6 S4 −948.218 0.100 S5 4440.119 19.600 1.49699 81.6 S6 −478.965 0.100 S7 355.717 24.300 1.49699 81.6 S8 −1197.673 0.100 S9 168.455 28.500 1.49699 81.6 S10 686.627 Variable S11 240.261 2.650 1.77249 49.6 S12* 58.196 12.668 S13 307.706 2.900 1.77249 49.6 S14 100.924 19.233 SiS −70.095 3.050 1.77249 49.6 S16 236.075 14.100 1.84666 23.8 S17 −126.479 Variable S18 −420.335 9.200 1.49699 81.6 S19 −81.355 0.126 S20 155.733 15.650 1.49699 81.6 S21 −98.523 2.750 1.80099 35.0 S22 −285.204 10.687 S23 76.070 7.900 1.49699 81.6 S24 118.043 Variable STOP Infinity 6.800 S26* −35.243 6.500 1.60674 45.1 S27 55.360 0.106 S28 55.900 4.050 1.75519 27.5 S29 155.439 4.934 S30 −63.039 5.050 1.80518 25.4 S31 −39.609 2.240 S32 56.818 10.900 1.45S99 90.3 S33 −43.388 2.150 1.80099 35.0 S34 −61.503 2.158 S35 107.501 2.100 1.80099 35.0 S36 29.896 11.600 1.49699 81.6 S37 166.103 78.890 S38 59.002 9.670 1.83741 25.4 S39 −405.826 20.924 S40 −22.134 19.750 1.80099 35.0 S41 −33.299 5.803 S42 −129.563 12.646 1.49699 81.6 S43 −52.914 0.152 S44 59.828 5.419 1.49699 81.6 S45 −209.080 0.100 S46 37.693 6.143 1.74099 52.7 S47 177.702 Variable S48 −106.846 1.600 1.83480 421 S49 21.576 6.448 550 −27.697 6.650 1.80099 35.0 S51 7367.260 0.829 S52 129.249 5.126 1.84583 24.0 S53 −46.358 Variable S54 538.505 1.500 1.80099 35.0 S55 95.344 11.395 1.60300 6S.5 S56 −60.650 Variable S57 87.009 5.185 1.48749 70.2 S58 −165.647 1.434 S59 −8S.3S7 1.500 1.80518 25.4 S60 −1236.715 0.100 S61 50.007 7.563 1.69472 54.5 S62 549.061 18.000 S63 Infinity 13.537 1.51633 64.1 S64 Infinity 2.051 S65 Infinity 33.841 1.60859 46.4 S66 Infinity Variable IMAGE Infinity Note: Maximum image diameter = 11.0 mm *Surface profiles of aspheric surfaces S12 and S26 are governed by the following conventional equation: $Z = {\frac{({CURV})Y^{2}}{1 + \left( {1 - {\left( {1 + K} \right)({CURV})^{2}Y^{2}}} \right)^{1/2}} + {(A)Y^{4}} + {B(Y)}^{6} + {(C)Y^{8}} + {(D)Y^{10}}}$ where: CURV = 1/(Radius of Surface) Y = Aperture height, measured perpendicular to optical axis K, A, B, C, D = Coefficients Z = Position of surface profile for a given Y value, as measured along the optical axis from the pole (i.e. axial vertex) of the surface. The coefficients for the surface S12 are: K = 0.0 A = 1.3820532e−007 B = −2.7133115e−011 C = −9.2535195e−015 D = 3.3313103e−018 The coefficients for the surface S26 are: K = −0.5520119 A = −1.0148386e−006 B = −5.9646048e−011 C = −1.3030573e−013 D = 3.2918363e−016 VARIABLE THICKNESS POSITIONS AND DATA P1 P2 P3 P4 P5 P6 P7 EFL 7.274 12.145 36.011 82.004 144.947 738.776 2095.406 F/No. 1.450 1.450 1.450 1.450 1.450 9.400 14.100 S10 3.154 50.878 126.861 163.460 167.963 167.403 168.654 S17 271.009 213.056 113.646 61.255 10.607 68.828 3.277 S24 2.350 12.345 35.982 51.876 97.922 40.276 104.616 S47 4.633 5.482 4.658 5.264 6.015 53.226 73.878 S53 105.364 104.868 105.482 104.798 103.775 14.725 2.050 S56 1.550 1.550 1.550 1.550 1.550 43.752 35.462 S66 4.969 4.799 4.853 4.815 5.202 4.818 5.114 Surface Groups Focal Lengths S1-S10 262.599 S11-S17 −50.895 S18-S24 98.756 S25-S47 37.686 S48-S53 −25.559 S54-S56 106.555 S57−S62 81.336 Surface Group Magnifications Surfaces P1 M′ P1 MP′ P2 M′ P2 MP′ P3 M′ P3 MP′ P4 M′ P4 MP′ S1-S10 0.000 0.805 0.000 0.626 0.000 0.337 0.000 0.191 S11-S17 −0.248 7.962 −0.323 7.245 −0.625 7.155 −1.136 9.531 S18-S24 −0.349 0.734 −0.431 0.633 −0.680 0.394 −0.831 0.233 S25-S47 −1.752 −0.293 −1.612 −0.293 −1.683 −0.293 −1.613 −0.293 S48-S53 −0.505 5.934 −0.574 4.957 −0.532 5.900 −0.571 5.176 S54-S56 −1.558 1.108 −1.529 1.487 −1.539 1.120 −1.533 1.378 S57-S62 0.233 1.240 0.235 3.217 0.234 1.263 0.234 2.205 Surfaces P5 M′ P5 MP′ P6 M′ P6 MP′ P7 M′ P7 MP′ S1-S10 0.000 0.130 0.000 0.184 0.000 0.120 S11-S17 −1.263 −8.111 −1.246 6.886 −1.285 −6.384 S18-S24 −1.324 −0.233 −0.748 0.350 −1.444 −0.301 S25-S47 −1.813 −0.293 −1.890 −0.293 −2.412 −0.293 S48-S53 −0.496 4.492 −3.524 0.483 −4.060 0.347 S54-S56 −1.600 1.750 −1.939 2.244 −1.904 1.880 S57-S62 0.230 −29.370 0.234 −0.833 0.231 −1.610 Where, P1 M′ is lens group magnification of lens group which equals (entrance marginal ray angle)/(exit marginal ray angle) and, P1 MP′ is lens group magnification which equals entrance principal ray angle/exit principal ray angle and so on, upto P7 M′ and P7 MP′; the first two characters representing position number, for example P1 M′ and P1 MP′ are for position 1.

TABLES FOR FIGS. 9A & 9B LENS SYSTEM OPTICAL PRESCRIPTION Glass Glass Surface Radius Thickness Index Dispersion OBJECT Infinity Variable S1 Infinity 50.000 S2 −621.758 5.169 1.69350 53.2 S3 457.301 Variable S4 −2452.883 4.799 1.80518 25.4 S5 599.599 Variable S6 911.220 25.082 1.45599 90.3 S7 −497.020 0.100 S8 −2000.000 0.000 S9 1000.000 0.000 S10 2062.549 12.736 1.49699 81.6 S11 −1165.481 Variable S12 963.440 19.740 1.49699 81.6 S13 −560.694 0.200 S14 382.994 19.312 1.49699 81.6 S15 −17187.180 0.200 S16 191.959 26.185 1.43875 95.0 S17 702.850 0.000 S18 324.818 Variable S19 130.133 3.120 1.77249 49.6 S20* 40.551 15.089 S21 87.300 2.500 1.77249 49.6 S22 70.260 14.709 S23 −76.831 2.730 1.77249 49.6 S24 108.868 11.313 1.84666 23.8 S25 −166.114 Variable S26 2466.515 12.326 1.49699 81.6 S27 −72.273 0.200 S28 114.639 17.864 1.49699 81.6 S29 −80.007 3.100 1.80099 35.0 S30 −402.245 0.200 S31 56.927 6.364 1.48749 70.2 532 83.100 Variable STOP Infinity 6.855 S34* −32.543 2.000 1.60311 60.7 S35 −178.894 11.407 S36 −41.737 3.274 1.84666 23.8 S37 −32.963 0.200 S38 49.510 12.747 1.49699 81.6 S39 −39.721 2.400 1.80099 35.0 S40 −53.729 0.200 S41 −163.422 1.850 1.80439 39.6 S42 26.111 9.221 1.49699 81.6 S43 −156.748 58.646 S44 44.245 2.533 1.80439 39.6 S45 1686.200 39.233 S46 −21.116 6.938 1.77249 49.6 S47 −21.969 14.095 S48 92.954 2.220 1.60300 65.5 S49 −59.449 0.200 S50 20.331 2.228 1.62229 53.2 S51 47.914 Variable S52 −116.378 0.950 1.83480 42.7 S53 34.369 3.756 S54 −16.771 0.950 1.81600 46.6 S55 −36.990 1.142 S56 −21.552 17.886 1.78469 26.3 S57 −26.412 Variable S58 −293.612 4.856 1.60311 60.7 S59 −78.391 0.200 S60 272.204 5.642 1.49699 81.6 S61 −126.344 0.200 S62 124.541 7.681 1.49699 81.6 S63 −102.092 2.500 1.80518 25.4 S64 −874.268 0.200 S65 400.000 0.000 S66 38.596 8.430 1.45599 90.3 S67 211.910 6.207 S68 Infinity 0.500 S69 123.725 2.000 1.81600 46.6 S70 39.478 7.176 S71 −84.356 2.000 1.74099 52.7 S72 36.196 18.326 1.84666 23.8 S73 210.724 0.984 S74 Infinity 7.645 S75 105.952 3.999 1.49699 81.6 S76 −91.250 0.200 S77 46.317 5.948 1.60300 65.5 S78 −69.543 1.500 1.84666 23.8 S79 166.511 22.000 S80 Infinity 13.200 1.51633 64.1 S81 Infinity 2.000 S82 Infinity 33.000 1.60859 46.4 S83 Infinity 0.000 S84 Infinity 0.000 IMAGE Infinity Note: Maximum image diameter = 11.0 mm *Surface profiles of asphenc surfaces S20 and S34 are governed by the following conventional equation: $Z = {\frac{({CURV})Y^{2}}{1 + \left( {1 - {\left( {1 + K} \right)({CURV})^{2}Y^{2}}} \right)^{1/2}} + {(A)Y^{4}} + {B(Y)}^{6} + {(C)Y^{8}} + {(D)Y^{10}}}$ where: CURV = 1/(Radius of Surface) Y = Aperture height, measured perpendicular to optical axis K, A, B, C, D = Coefficients Z = Position of surface profile for a given Y value, as measured along the optical axis from the pole (i.e. axial vertex) of the surface. The coefficients for the surface S20 are: K = −0.3254663 A = −3.65160e−007 B = −1.14704e−010 C = −5.60564e−014 D = −5.86283e−018 The coefficients for the surface S34 are: K = 0.348034 A = 1.350560e−006 B = 2.453070e−009 C = −2.820340e−012 D = 4.745430e−015 VARIABLE THICKNESS POSITIONS AND DATA P1 P2 P3 P4 35 P6 EFL 7.278 7.278 7.278 8.817 12.199 18.641 F/No. 1.749 1.749 1.749 1.749 1.749 1.749 SO Infinity 5322.600 2499.900 Infinity Infinity Infinity S3 17.233 50.424 82.285 17.233 17.233 17.233 S5 3.856 8.913 13.211 3.856 3.856 3.856 S11 74.605 36.357 0.200 74.605 74.605 74.605 S18 0.200 0.200 0.200 26.070 64.733 106.272 S25 300.191 300.191 300.191 272.377 230.274 183.410 S32 1.334 1.334 1.334 3.266 6.708 12.035 S51 1.647 1.647 1.647 1.647 1.647 1.647 S57 80.778 80.778 80.778 80.778 80.778 80.778 VARIABLE THICKNESS POSITIONS AND DATA P7 P8 P9 P10 P11 P12 EFL 32.734 60.449 94.190 123.985 206.250 284.791 F/No. 1.749 1.749 1.890 2.020 2.160 2.700 SO Infinity Infinity Infinity Infinity Infinity Infinity S3 17.233 17.233 17.233 17.233 17.233 17.233 S5 3.856 3.856 3.856 3.856 3.856 3.856 S11 74.605 74.605 74.605 74.605 74.605 74.605 S18 148.849 183.007 201.036 209.783 216.511 215.851 S25 132.062 85.948 57.616 42.322 21.856 15.570 S32 20.806 32.763 43.065 49.609 63.170 70.310 S51 1.647 1.647 2.130 3.050 8.806 15.438 S57 80.778 80.778 80.294 79.375 73.618 66.987 VARIABLE THICKNESS POSITIONS AND DATA P13 P14 P15 P16 P17 EFL 717.193 2092.160 2092.160 2092.160 2092.160 F/No. 5.200 13.750 13.750 13.750 17.490 SO Infinity Infinity 8708.000 4050.000 2499.900 S3 17.233 17.233 37.759 59.403 82.285 S5 3.856 3.856 7.178 10.305 13.211 S11 74.605 74.605 50.757 25.988 0.200 S18 211.275 208.261 208.261 208.261 208.261 S25 5.736 0.200 0.200 0.200 0.200 S32 84.680 93.262 93.262 93.262 93.262 S51 39.946 82.225 82.225 82.225 82.225 S57 42.480 0.200 0.200 0.200 0.200 Surface Groups Focal Lengths S2-S3 −379.209 S4-S5 −597.975 S6-S11 484.131 S12-S18 229.394 S2-S18 262.190 S19-S25 −49.050 S26-S32 79.931 S33-S51 41.254 S52-S57 −26.810 S58-S79 70.920 Surface Group Magnifications Surfaces P1 M′ P1 MP′ P2 M′ P2 MP′ P3 M′ P3 MP′ P4 M′ P4 MP′ S2-S3 0.000 1.732 0.066 1.710 0.129 1.696 0.000 1.971 S4-S5 0.599 1.754 0.594 1.563 0.59 1.425 0.599 2.388 S6-S11 2.150 0.529 2.229 0.608 2.304 0.682 2.150 0.374 S12-S18 −0.537 0.642 −0.537 0.642 −0.537 0.642 −0.537 0.53 S2-S18 0.000 1.030 −0.047 1.043 −0.094 1.058 0.000 0.934 S19-S25 −0.185 8.447 −0.185 8.447 −0.185 8.447 −0.206 7.952 S26-S32 −0.252 0.756 −0.252 0.756 −0.252 0.756 −0.252 0.731 S33-S51 −1.446 −0.378 −1.446 −0.378 −1.446 −0.378 −1.442 −0.378 S52-S57 −0.673 6.392 −0.673 6.392 −0.673 6.392 −0.676 6.392 S58-S79 −0.611 0.966 −0.611 0.966 −0.611 0.966 −0.611 0.966 Surfaces P5 M′ P5 MP′ P6 M′ P6 MP′ P37 M′ P7 MP′ P8 M′ P8 MP′ S2-S3 0.000 2.695 0.000 6.440 0.000 −4.655 0.000 −1.279 S4-S5 0.599 −24.64 0.599 −0.414 0.599 0.216 0.599 0.403 S6-S11 2.150 −0.033 2.150 −1.271 2.150 −127.8 2.150 4.484 S12-S18 −0.537 0.365 −0.537 0.187 −0.537 0.004 −0.537 −0.147 S2-S18 0.000 0.788 0.000 0.633 0.000 0.473 0.000 0.341 S19-S25 −0.245 7.233 −0.31 6.531 −0.424 6.046 −0.601 6.421 S26-S32 −0.319 0.688 −0.386 0.622 −0.496 0.512 −0.646 0.362 S33-S51 −1.445 −0.378 −1.448 −0.378 −1.448 −0.378 −1.449 −0.378 S52-S57 −0.673 6.392 −0.671 6.392 −0.671 6.392 −0.67 6.392 S58-S79 −0.611 0.966 −0.612 0.966 −0.612 0.966 −0.612 0.966 Surfaces P9 M′ P9 MP′ P10 M′ P10 MP′ P11 M′ P11MP′ P12 M′ P12MP′ S2-S3 0.000 −0.736 0.000 −0.549 0.000 −0.387 0.000 −0.365 S4-S5 0.599 0.468 0.599 0.496 0.599 0.522 0.599 0.526 S6-S11 2.150 3.296 2.150 2.964 2.150 2.701 2.150 2.668 S12-S18 −0.537 −0.234 −0.537 −0.279 −0.537 −0.330 −0.537 −0.338 S2-S18 0.000 0.265 0.000 0.225 0.000 0.180 0.000 0.173 S19-S25 −0.771 8.327 −0.894 11.79 −0.983 −18.95 −1.004 −14.68 S26-S32 −0.770 0.233 −0.846 0.152 −1.064 −0.084 −1.092 −0.107 S33-S51 −1.431 −0.378 −1.406 −0.378 −1.344 −0.378 −1.359 −0.378 S52-S57 −0.692 5.731 −0.728 4.790 −0.916 2.531 −1.194 1.491 S58-S79 −0.611 1.263 −0.611 2.227 −0.611 −2.992 −0.610 −1.604 Surfaces P13M′ P13MP′ P14M′ P14MP′ P15M′ P15MP′ P16M′ P16MP′ S2-S3 0.000 −0.351 0.000 −0.348 0.041 −0.294 0.085 −0.24 S4-S5 0.599 0.529 0.599 0.529 0.596 0.529 0.593 0.529 S6-S11 2.150 2.646 2.150 2.642 2.199 2.691 2.250 2.742 S12-S18 −0.537 −0.344 −0.537 −0.345 −0.537 −0.345 −0.537 −0.345 S2-S18 0.000 0.169 0.000 0.168 −0.029 0.145 −0.061 0.12 S19-S25 −0.919 −5.386 −0.870 −3.955 −0.869 −3.955 −0.869 −3.955 S26-S32 −1.351 −0.287 −1.561 −0.395 −1.561 −0.395 −1.561 −0.395 S33-S51 −1.719 −0.378 −2.606 −0.378 −2.61 −0.378 −2.612 −0.378 S52-S57 −2.093 0.631 −3.758 0.316 −3.685 0.316 −3.626 0.316 S58-S79 −0.613 −1.659 −0.600 −7.955 −0.610 −7.955 −0.619 −7.955 Surfaces P17M′ P17MP′ S2-S3 0.129 −0.183 S4-S5 0.590 0.528 S6-S11 2.304 2.795 S12-S18 −0.537 −0.345 S2-S18 −0.094 0.093 S19-S25 −0.869 −3.955 S26-S32 −1.561 −0.395 S33-S51 −2.612 −0.378 S52-S57 −3.629 0.316 S58-S79 −0.618 −7.955 Where, P1 M′ is lens group magnification of lens group which equals (entrance marginal ray angle)/(exit marginal ray angle) and, P1 MP′ is lens group magnification which equals entrance pricipal ray angle/exit principal ray angle and so on, upto P17 M′ and P17 MP′; the first two characters representing position number, for example P1 M′ and P1 MP′ are for position 1. The group of elements defined by surfaces 69 through 73 is translated in a direction perpendicular to the optical axis to compensate for image vibration

In the lens system optical prescriptions provided above for each of the four embodiments, each surface of a lens element identified in the left hand column (“Surface”), the radius of that surface in the second column (“Radius”), the thickness on the optical axis between that surface and the next surface, whether glass or air, in the third column (“Thickness”), the refractive indices of the glass lens elements set forth in the fourth column (“Glass Index”), and the dispersion values for the lens elements (“Glass Dispersion”) set forth in the fifth column. The surface numbers in the first column “Surface” represent the surfaces numbered from left-to-right in the Figs. in the conventional manner, namely from object space to image space.

In the left hand or “Surface” column of each lens system optical prescription provided above, the object to be imaged (e.g., photographed) is identified as “OBJECT”, the adjustable iris or stop is identified as “STOP”, and the final image is identified as “IMAGE”. The adjustable spaces between lens elements, such as on either side of movable zoom groups, are identified as “Variable” in the third or Thickness column of the lens system optical prescription. The EFL, Radius and Thickness dimensions are given in millimeters with the Thickness being the distance after that surface on the optical axis. When two surfaces of adjacent elements have the same radius and are coincident, as in a doublet or triplet, only one surface is identified in the first or “Surf” column.

For each of the four embodiments, Aspheric Coefficients for each of the aspheric surfaces are provided following the table of optical prescriptions.

In addition, for each of the four embodiments, tables of the variable thickness positions for various surfaces in each lens system optical prescription are provided which identify positions in the format “Px” for various surfaces (corresponding to entries in the Surface column of the optical prescription tables). The effective focal length (EFL) and the “f” number (F/No.) are also provided for each position.

Now each of the four embodiments of FIGS. 6A-9B will be described briefly to identify some of their differences. The embodiment of FIGS. 6A and 6B has an effective focal length range of about 7.25 mm to 900 mm, which provides a zoom ratio of about 125:1, while using three movable zoom lens groups, namely, Zoom 1, Zoom 2, and Zoom 3, with a focus lens group Focus at the object space end of the lens. The Zoom 3 group actually is comprised of two groups of elements that have a small amount of movement between surfaces S47 and S48 (compare FIGS. 6A and 6B). The embodiment of FIGS. 7A and 7B has an effective focal length range of about 7.27 mm to 2088 mm, which provides a zoom ratio of about 287:1, with four movable zoom lens groups (Zoom 1, 2, 3 and 4) and a focus lens group. The embodiment of FIGS. 8A and 8B has an effective focal length range of about 7.27 mm to 2095 mm, which also provides a zoom range of about 287:1, with four moving zoom lens groups and a focus lens group, which is very similar to the performance of the lens embodiment of FIGS. 7A and 7B. Similarly, the embodiment of FIGS. 9A and 9B has an effective focal length range of about 7.27 mm to 2092 mm, which also provides a zoom ratio of about 287:1, but uses only three moving zoom lens groups. Each of these four embodiments includes plural aspheric surfaces with the embodiments of the FIGS. 8A-8B and 9A-9B having only two such surfaces while the embodiment of FIGS. 7A-7B includes eight such surfaces, as indicated in the lens system optical prescriptions. The embodiment of FIGS. 9A and 9B also includes optical image stabilization lens elements near the camera end of the lens system similar to those included in the embodiment of FIGS. 10-62, which will be described below.

Detailed Description of the Embodiment of FIGS. 10-62. As noted above in the section entitled “Brief Description of the Drawings,” FIGS. 10-62 all relate to a single embodiment of the present invention that is directly and immediately applicable to the broadcast television market, although other markets are also available and various other embodiments and modifications of the invention may be more applicable to other markets. This embodiment of the compound zoom lens system of this invention has a zoom range of approximately 7 mm to 2100 mm in focal length, thereby providing a zoom ratio of about 300:1, which is more than three times the zoom ratio presently available in broadcast television zoom lens systems. Referring more particularly to the optical diagram of FIG. 10, the zoom lens system ZL is comprised of a focus lens group FG, a front zoom group FZG and a rear zoom group RZG. For the description of this embodiment, the lens system's stop is used as a divider between the “front” and “rear” of the lens. In terms of the terminology used in the “Description of Various Features of the Invention and the Disclosed Embodiments” set forth above, the focus lens group FG is the focus unit, the front zoom group FZG is the first optical unit, and the rear zoom group RZG includes a pupil imaging unit and an image stabilization unit, as well as the second optical unit.

The focus group FG is comprised of seven lens elements 1-7 with the front lens element 1 being stationary whereby the lens may be sealed at the front by fixing and sealing element 1 to the lens barrel (not shown). Lens element 2 comprises a first focus group FG1 and lens elements 3 and 4 comprise a second focus group FG2, both of which groups are independently movable for achieving the desired focus at each focal length. Elements 5-7 of the focus group FG are stationary.

The front zoom group FZG has a first zoom group ZG1 comprised of lens elements 8-11 and a second zoom group ZG2 comprised of lens elements 12-15, both of which zoom groups are independently movable. An iris or aperture stop STOP is positioned between the second zoom group ZG2 and a first group RG1 that forms the front portion of the rear zoom group RZG.

First group RG1 is comprised of lens elements 16-25, which remain stationary. The intermediate image is formed between lens elements 22 and 23 in the first group RG1. Although all of the lens elements 16-25 of this first group RG1 remain stationary at all times, the intermediate image moves along the optical axis between lens elements 22 and 23 at the longer focal lengths without touching either of those elements during the zooming of the lens system between the maximum and minimum focal lengths. The next lens group of the rear zoom group RZG is a third zoom group ZG3 comprised of lens elements 26-28 that are movable axially. Next within the rear zoom group RZG is a second group RG2 comprised of lens elements 29-33, which are stationary. The next elements in the rear zoom group RZG comprise a stabilization group SG having a radial decentralization group SG1 with lens elements 34-36 and an axially adjustable group SG2 with lens elements 37-39. The three zoom groups ZG1, ZG2 and ZG3 are independently movable along the optical axis for developing the full range of the focal lengths of about 7 mm to 2100 mm. Finally, although they are not part of the zoom lens system per se, FIG. 10 also illustrates two prism blocks 40 and 41 that emulate the conventional three CCD ⅔″ detectors of a video camera for completing the optical diagram from object space to the final image.

The first or decentralization stabilization group SG1 is movable radially from the system's optical axis in any direction by about 0.5 mm or more in response to sensed vibrations of the lens to maintain the final image at the image plane in a stabilized location. The sensing of vibrations and the movement of group SG1 may be accomplished by any conventional means such as an accelerometer, a processor and a motor controlled by the processor in a closed loop system on a continuous basis. The second or axial stabilization group SG2 is axially movable for axial adjustment of about 1.25 mm or more in either direction for back focus adjustment. The second stabilization group SG2 may also be moved axially forward a greater amount for extended close focus at short focal lengths of the lens. The light rays between the first stabilization group SG1 and the second stabilization group SG2, i.e. between lens elements 36 and 37, are substantially collimated whereby the movements of those two groups for accomplishing stabilization, extending the close focus and adjusting the back focus do not cause any significant deterioration of the final image.

The decentralization stabilization group SG1 may also be used for creating special effects by causing the lens group SG1 to move radially in a shaking pattern to thereby simulate the shaking caused, for example, by an earthquake, a moving vehicle or explosions in a war movie. Such special effects can also be produced by moving the lens group SG2 axially in an oscillatory fashion, which slightly defocuses the picture. Radial movement of SG1 can also be combined with axial movement of SG2 to create a different special effect.

The complete lens design of the zoom lens system ZL for the embodiment of FIGS. 10-62 is set forth below in the tables generally entitled “Tables for FIGS. 10 thru 62.” The Lens System Optical Prescription table is similar to the foregoing lens prescriptions for the zoom lenses of FIGS. 6A-9B. A more detailed explanation of the tables is provided following the tables. TABLES FOR FIGS. 10 thru 62 LENS SYSTEM OPTICAL PRESCRIPTION Semi Surface Radius Thickness Glass Name Manufacturer Aperture OBJECT Infinity Variable S1 Infinity 50.000 142.85 S2 −553.385 5.200 SLAL13 OHARA 111.77 S3 436.730 Variable 103.81 S4 −1545.910 4.900 STIH6 OHARA 102.97 SS 682.341 Variable 101.63 S6 1644.762 19.482 SFPL52 OHARA 101.59 S7 −467.261 0.730 101.38 S8 −2000.000 0.000 99.83 S9 4000.000 0.000 99.22 S10 1463.863 12.601 SFPLS1 OHARA 98.87 S11 −1094.948 Variable 98.22 S12 1092.461 20.386 SFPL51 OHARA 100.60 S13 −480.155 0.730 101.05 S14 362.425 21.232 SFPL51 OHARA 101.85 S15 −14624.000 0.730 101.37 S16 181.063 24.150 SFPL53 OHARA 97.84 S17 477.885 0.000 96.42 S18 324.818 Variable 95.12 S19 208.678 3.120 SLAH66 OHARA 38.27 S20* 40.147 6.111 32.19 S21 67.136 3.150 SLAH59 OHARA 32.03 S22 56.870 14.527 30.64 S23 −98.690 2.730 SLAH66 OHARA 30.54 S24 90.992 12.5065 TIH53 OHARA 33.74 S25 −174.619 Variable 34.43 S26 764.771 14.926 SFPL52 OHARA 36.34 S27 −66.842 0.400 36.91 S28 133.738 17.704 SFPL51 OHARA 36.84 S29 −69.988 3.100 SLAM66 OHARA 36.62 S30 −1580.221 0.400 36.97 S31 65.214 9.613 SNSL36 OHARA 37.33 S32 129.561 Variable 36.67 STOP Infinity 8.811 20.27 S34* −36.392 2.044 SBSM14 OHARA 20.44 S35 −425.016 6.131 21.70 S36 −43.308 5.233 STIH53 OHARA 21.88 S37 −33.861 0.200 22.78 S38 47.203 13.980 SFPL51 OHARA 22.84 S39 −41.565 2.400 SLAM66 OHARA 22.59 S40 −56.845 0.200 22.47 S41 −109.533 1.950 SLAH63 OHARA 21.13 S42 31.532 10.159 SFPL51 OHARA 19.56 S43 −173.403 45.721 19.51 S44 47.891 4.513 SLAH53 OHARA 15.23 S4S −2514.287 41.843 14.84 S46 −23.807 9.483 SLAH59 OHARA 8.45 S47 −24.610 12.719 9.87 S48 61.223 3.114 SFPL51 OHARA 8.86 S49 −45.071 0.150 8.71 S50 24.918 3.242 SBSM9 OHARA 8.83 S51 −516.606 Variable 8.67 S52 −72.073 1.059 SLAL54 OHARA 7.15 S53 23.513 2.783 6.65 S54 −18.951 0.900 SLAH59 OHARA 6.54 S55 −57.174 1.347 6.84 S56 −21.150 21.292 SLAH60 OHARA 6.98 S57 −31.181 Variable 12.67 S58 −138.459 4.401 SBAL22 OHARA 23.12 S59 −75.648 0.300 23.54 S60 606.713 5.842 SFPL51 OHARA 23.89 561 −96.488 0.300 23.97 S62 113.288 7.382 SFPL51 OHARA 23.55 S63 −97.742 2.500 STIH6 OHARA 23.30 S64 −366.723 0.300 23.05 S65 400.000 0.000 22.80 S66 38.760 8.585 SFPL52 OHARA 21.88 S67 269.438 5.901 21.07 S68 115.000 0.450 18.30 S69 94.072 1.770 SLAL54 OHARA 18.00 S70 35.982 7.000 16.65 S71 −90.502 2.010 SLAL8 OHARA 16.35 S72 29.972 6.150 STIH53 OHARA 16.01 S73 82.308 2.725 15.75 S74 79.000 9.670 15.78 S75 76.232 6.100 SPHM52 OHARA 15.87 S76 −75.003 0.761 15.66 S77 45.420 7.170 SFSL5 OHARA 14.38 S78 −45.317 1.500 STIH53 OHARA 13.58 S79 348.342 18.544 12.98 S80 Infinity 13.200 SBSL7 OHARA 10.30 S81 Infinity 2.000 9.00 S82 Infinity 33.000 BAF52 SCHOTT 8.70 S83 Infinity 0.000 5.69 S84 Infinity 0.000 IMAGE Infinity 0.000 Note: Maximum image diameter = 11.0 mm *Surface profiles of aspheric surfaces S20 and S34 are govemed by the following conventional equation: $Z = {\frac{({CURV})Y^{2}}{1 + \left( {1 - {\left( {1 + K} \right)({CURV})^{2}Y^{2}}} \right)^{1/2}} + {(A)Y^{4}} + {B(Y)}^{6} + {(C)Y^{8}} + {(D)Y^{10}}}$ where: CURV = 1/ (Radius of Surface) Y = Aperture height, measured perpendicular to optical axis K, A, B, C, D = Coefficients Z = Position of surface profile for a given Y value, as measured along the optical axis from the pole (i.e. axial vertex) of the surface. The coefficients for The coefficients for the surface S20 are: the surface S34 are: K = −0.3564030 K = 0.4304790 A = −8.06827e−07 A = 9.57697e−07 B = −2.15109e−10 B = 1.31318e−09 C = −6.36649e−14 C = −1.45592e−12 D = −3.89379e−18 D = 3.19536e−15 VARIABLE THICKNESS POSITIONS AND DATA P1 P2 P3 P4 P5 P6 P7 EFL 7.391 8.820 12.231 19.219 32.730 64.634 −93.220 F/No. 1.949 1.949 1.949 1.949 1.949 1.949 2.010 S0 Infinity Infinity 5322.630 2499.896 Infinity 5322.630 Infinity S3 19.882 19.882 49.699 78.333 19.882 49.699 19.882 S5 5.690 5.690 10.880 15.384 5.690 10.879 5.690 S11 71.522 71.522 36.516 3.376 71.522 36.516 71.522 S18 1.350 26.428 67.051 110.745 155.094 189.151 203.856 S25 319.660 292.522 247.857 197.854 142.790 92.653 65.474 S32 9.625 11.684 15.727 22.036 32.751 48.830 61.304 S51 1.498 1.498 1.498 1.498 1.498 1.498 2.823 S57 63.257 63.257 63.257 63.257 63.257 63.257 61.933 VARIABLE THICKNESS POSITIONS AND DATA P8 P9 P10 P11 P12 P13 P14 EFL 145.184 206.228 490.401 717.511 2065.045 −3694.934 −920.968 F/No. 2.090 2.360 2.840 5.600 13.064 13.064 13.064 50 5322.630 Infinity 5322.630 Infinity Infinity 8708.002 4050.000 S3 49.699 19.882 49.699 19.882 19.882 38.428 57.882 S5 10.879 5.690 10.879 5.690 5.690 9.057 12.294 S11 36.516 71.522 36.516 71.522 71.522 49.608 26.917 S18 210.392 215.814 218.877 223.339 224.980 224.980 224.980 S25 50.046 33.074 24.338 10.235 1.719 1.719 1.719 S32 70.197 81.746 87.419 97.063 103.934 103.934 103.934 S51 4.711 9.572 14.559 31.080 63.536 63.536 63.536 S57 60.044 55.183 50.196 33.675 1.220 1.220 1.220 VARIABLE THICKNESS POSITIONS AND DATA P15 P16 P17 P18 P19 P20 EFL −509.031 −1739.084 −387.928 7.227 114.357 377.554 F/No. 16.750 5.600 5.600 1.949 2.010 2.360 S0 2499.896 5322.630 2499.896 2499.896 2499.896 2499.896 S3 78.333 49.699 78.333 78.333 78.333 78.333 S5 15.384 10.879 15.384 15.384 15.384 15.384 S11 3.376 36.516 3.376 3.376 3.376 3.376 S18 224.980 223.339 223.339 1.350 203.856 215.814 S25 1.719 10.235 10.235 319.660 65.474 33.074 S32 103.934 97.063 97.063 9.625 61.304 81.746 S51 63.536 31.080 31.080 1.498 2.823 9.572 S57 1.220 33.675 33.675 63.2S7 61.933 55.183 Surface Groups Focal Lengths S2-S3 −349.648 S4-S5 −581.962 S6-S7 798.201 S10-S11 1258.758 S12-S13 672.072 S14-S15 709.848 S16-S17 646.676 S19-S20 −64.565 S21-S22 −526.211 S23-S25 −554.999 S26-S27 135.208 S28-S30 113230.702 S31-S32 240.348 S34-S35 −65.863 S36-S37 144.623 S38-S40 60.255 S41-S43 −70.987 S44-S45 58.010 S46-S47 205.873 S48-S49 52.593 S50-S51 38.634 S52-S53 −27.000 S54-S55 −34.933 S56-S57 −2495.053 S58-S59 284.851 S60-S61 167.476 S62-S64 292.466 S66-S67 97.878 S69-S70 −90.217 S71-S73 −72.295 S75-S76 61.902 S77-S79 1261.227 580-S81 Infinity S82-S83 Infinity

The Lens System Optical Prescription table comprises the “Listing” for the lens specification and numerically lists each lens “SURFACE” in the left-hand column, but also includes dummy surfaces used in the design such as dummy surfaces S1, S8, S9, S118, S65, S74 and S84. The second column “Radius” lists the radius of the respective surfaces with a negative radius indicating that the center of curvature is to the left. The third column “Thickness” lists the thickness of the lens element or space from that surface to the next surface on the optical axis. The fourth column “Glass Name” lists the type of glass and the fifth column “Manufacturer” lists the manufacturer of each glass material. The fifth column “Semi Aperture” provides a measurement of half the aperture diameter for each lens element.

In the left-hand column the legend “OBJECT” means the object to be imaged (e.g., photographed), the legend “STOP” means the iris or stop, and the legend “IMAGE” means the final image. Each of the surfaces is identified by a numeral preceded by “S” to distinguish the surfaces from the numerals that identify the lens elements set forth on the subsequent pages comprising the 39 glass lens elements described above with respect to FIG. 10 and prisms 40 and 41 of the detector.

It should be noted that each of the thickness dimensions set forth in the third column of the table listing the surfaces is the element thickness or air space along the optical axis for the zoom lens system ZL set to the shortest focal lens (7.39 mm EFL) and focused at infinity. The air spaces adjacent the moving lens groups obviously will change in “thickness” for other focal lengths and focus distances.

For each aspheric surface, Aspheric Coefficients are provided following the table of optical prescriptions.

FIGS. 11-30 illustrate 20 representative positions for the zoom lens system of FIG. 10. These 20 positions are listed in the following Table of Lens Positions: TABLE OF LENS POSITIONS Paraxial EFL (mm) Focus Distance (mm) To Object* @ Infinity Focus “F” No. INF. 8758 5372 4100 2550 7.3909 1.95 1 18 8.8200 1.95 2 12.1938 1.95 3 18.6371 1.95 4 32.7300 1.95 5 60.2959 1.95 6 93.2199 2.01 7 19 127.2902 2.09 8 206.2278 2.36 9 20 297.4279 2.84 10 717.5114 5.60 11 16 17 2065.0447 13.06 12 13 14  15# *The Focus Distance is measured to the Object from the first refractive surface of the zoom lens system. #The “F” No. equals 16.75 at this position.

The twenty (20) positions were selected as representative of extreme positions of focal length and focus distance, as well as intermediate positions, for establishing the representative performances of the zoom lens system ZL of FIG. 10. In other words, position 1 is at the minimum paraxial focal length (wide angle) of about 7.4 mm and focused at infinity whereas position 18 is focused at 2550 mm (about eight feet) for the same focal length. Similarly, position 12 represents the longest paraxial focal length of about 2065 mm at infinity focus whereas position 15 represents the focus at 2550 mm at the same paraxial focal length. The paraxial EFL in the first column is at infinity focus. The “f” numbers are at any given focus and at full aperture. The 12 different focal lengths provide representative focal lengths over the full range of the zoom lens system ZL. Also, it should be noted that the actual field of view as a result of distortion and the available physical overtravel of the zoom groups beyond data in the lens system optical prescription set forth below produces an apparent focal length range of substantially 7.0 mm to 2100 mm, i.e. a zoom ratio of about 300:1, with the distortion primarily influencing the reduction in the minimum paraxial EFL and the overtravel primarily influencing the increase in the maximum paraxial EFL. At 2100 mm EFL with focus set at eight feet, the magnification is about 1.33:1.00 (object to image size). The nominal lens design for the embodiment of FIGS. 10-62 as reflected in the lens optical prescription tables for FIGS. 10-62 is given at 77° F. (25° C., 298 K) and standard atmospheric pressure (760 mm Hg).

Referring now to FIGS. 11-30, the twenty positions 1-20 set forth in the foregoing lens system optical prescription and the preceding TABLE OF LENS POSITIONS are shown in that order. For example, FIG. 11 is an optical diagram of the lens elements in Position 1, namely, a paraxial effective focal length (EFL) of 7.391 mm and focused at infinity, wherein the first and second focus groups FG1 and FG2 are closely separated, the first and second zoom groups ZG1 and ZG2 are widely separated, and the third zoom group ZG3 is in its most forward position. On the other hand, FIG. 25 is the optical diagram representing Position 15 with the largest focal length and shortest focus distance, wherein the first and second focus groups FG1 and FG2 are both in their rearmost position, the first and second zoom groups ZG1 and ZG2 are in a closely spaced position but intermediately spaced between adjacent lens groups, and the third zoom group ZG3 is in the rearmost position.

FIGS. 31-34 are enlarged optical diagrams of only the seven focus group FG elements 1-7 and illustrate representative Positions 1, 18, 12 and 15, respectively. It should be noted that while the lens element positions in FIGS. 32 and 34 are the same, representing the focus distance of 2550 mm, the ray tracings are different because of the difference in the paraxial focal lengths from the minimum of about 7.4 mm in FIG. 32 to the maximum of about 2065 mm in FIG. 34.

FIGS. 35 and 36 are enlarged optical diagrams illustrating the last lens element 7 of the focus group FG and the first and second zoom groups ZG1 and ZG2 in Positions 1 and 12, respectively, for the minimum and maximum paraxial focal lengths, respectively. Similarly, FIGS. 37 and 38 represent the rear zoom group RZG with the third zoom group ZG3 in the forwardmost and rearmost Positions 1 and 12 representing the minimum and maximum paraxial focal length positions, all respectively.

Referring now to FIGS. 39-58, the ray aberration graphs for Positions 1-20, respectively, are shown in a conventional manner by five separate graphs with the maximum field height at the top and zero field height at the bottom and for five wavelengths, as listed thereon. As will readily appear to those skilled in the art, these performance curves establish that in all 20 positions the zoom lens system performs exceptionally well for current broadcast television NTSC quality and exceptionally well for HDTV broadcast television quality. While FIG. 50 representing Position 12, illustrates wide variations in the ray aberrations at this focal length and focused at infinity, the performance is satisfactory because the modulation transfer function is close to the diffraction limit. Similarly, FIGS. 52 and 53, representing Positions 14 and 15, respectively, illustrate widely varying ray aberrations but are still acceptable relative to diffraction limits for these close focus and long focal length positions.

Referring now to FIG. 59, the cam graph for the first and second focus groups FG1 and FG2 are shown (left and right, respectively) for the full range of focus travel thereof from infinity to close focus, with object space being to the left. The first and second focus groups FG1 and FG2 move separately and not at precisely the same rate, even though the solid cam lines in FIG. 59 look nearly parallel. The crosshatched portions at the top and bottom of FIG. 59 allow for temperature changes, manufacturing tolerances and fabrication adjustments. Similarly, FIG. 60 illustrates the cam graphs for the three zoom groups ZG1, ZG2 and ZG3 from left to right, respectively, and it is readily apparent that all three zoom groups move independently, although coordinated to achieve the desired focal lengths continuously over the entire range. FIG. 61 is a graph of the “f” number of the open stop relative to the paraxial effective focal length. Similarly, FIG. 62 is a graph of the full aperture full stop diameter relative to the paraxial effective focal length throughout the full range thereof.

Detailed Description of Other Embodiments. FIGS. 63 and 64 illustrate an example of another embodiment of the present invention. This embodiment of the zoom lens system is very similar to the embodiment of FIGS. 8A and 8B, except that a binary (diffractive) surface is provided. Specifically, a binary surface is provided on the front surface (surface No. 3 in the prescription) of the second lens element. The lens system optical prescription is set forth below in the tables generally entitled “Tables for FIGS. 63 and 64.” A more detailed explanation of the tables is provided following the tables. TABLES FOR FIGS. 63 and 64 LENS SYSTEM OPTICAL PRESCRIPTION Glass Surface Radius Thickness Name OBJECT Infinity Infinity S1 −731.222 10.000 LASF32 S2 390.798 15.991 S3# 827.075 22.500 BK7 S4 -1021.418 0.100 S5 −1257.463 −19.600 BK7 S6 −780.160 0.100 S7 436.979 24.300 BK7 S8 -835.454 0.100 S9 −170.301 28.500 BK7 S10 655.827 Variable S11 278.083 2.650 S-LAH66 S12* 60.022 −12.668 S13 277.706 2.900 S-LAH66 S14 98.325 −19.233 S15 −70.105 3.050 S-LAH66 S16 234.965 −14.100 S-TIH53 S17 −127.001 Variable S18 −404.763 9.200 S-FPL51 S19 −80.933 0.126 S20 −157.360 −15.650 S-FPL51 S21 −99.532 2.750 S-LAM66 S22 −284.625 −10.687 S23 76.300 7.900 S-FPL51 S24 −118.669 Variable STOP Infinity 6.800 S26* −34.999 6.500 BAF4 S27 54.435 0.106 S28 55.347 4.050 S-TIH4 S29 −158.504 4.934 S30 −64.093 5.050 S-TIH6 S31 −39.812 2.240 S32 56.945 −10.900 S-FPLS2 S33 −43.914 2.150 S-LAM66 S34 −61.923 2.158 S35 −106.356 2.100 S-LAM66 S36 30.350 −11.600 S-FPL51 S37 −151.277 78.890 S38 57.056 9.670 SF6 S39 −603.641 20.924 S40 −22.693 −19.750 S-LAM66 S41 −34.224 5.803 S42 −129.563 −12.646 S-FPL51 S43 −52.914 0.152 S44 59.828 5.419 S-FPL51 S45 −209.080 0.100 S46 37.693 6.143 S-LAL61 S47 −177.702 Variable S48 −106.846 −1.600 S-LAH55 S49 21.S76 6.448 S50 −27.697 6.650 S-LAM66 S51 7367.260 0.829 S52 −129.249 5.126 S-TIH53 S53 −46.358 Variable S54 538.505 −1.500 S-LAM66 S55 95.344 −11.395 S-PHM53 S56 −60.650 Variable S57 87.009 5.185 S-FSL5 S58 −165.647 −1.434 S59 −85.357 −1.500 S-TIH6 S60 −1236.715 0.100 S61 50.067 7.563 S-LAL14 S62 539.692 −18.000 S63 Infinity −13.537 S-BSL7 S64 Infinity 2.051 S65 Infinity 33.841 BAF52 S66 Infinity Variable IMAGE Infinity Note: Maximum image diameter = 11.0 mm *Surface profiles of aspheric surfaces S12 and S26 are governed by the following conventional equation: $Z = {\frac{({CURV})Y^{2}}{1 + \left( {1 - {\left( {1 + K} \right)({CURV})^{2}Y^{2}}} \right)^{1/2}} + {(A)Y^{4}} + {B(Y)}^{6} + {(C)Y^{8}} + {(D)Y^{10}}}$ where: CURV = −1/(Radius of Surface) Y = Aperture height, measured perpendicular to optical axis K, A, B, C, D = Coefficients Z = Position of surface profile for a given Y value, as measured along the optical axis from the pole (i.e. axial vertex) of the surface. The coefficients for The coefficients for the surface S12 are: the surface S26 are: K = 0.01925737 K = −0.5574845 A = −1.3531387e−007 A = −1.0833227e−006 B = −1.5274225e−011 B = −9.1904879e−011 C = −2.0209982e−014 C = −1.4775967e−013 D = 5.4753514e−0i8 D = 6.5701323e−016 # Surface profile of binary surface S3 is governed by the following conventional equation: Added Phase = A₁p² + A₂p⁴ + A₃p⁶ + A₄p⁸ + A₅p¹⁰ where: A1, A2, A3, A4 and A5 are coefficients and p is the normalized radial coordinate at the surface. The normalizing factor is set at unity and the p's become simply radial coordinates. A1 = −0.14123699 A2 = −8.7028052e−007 A3 = −1.2255122e−010 A4 = 5.9987370e−015 A5 = −1.2234791e−019 VARIABLE THICKNESS POSITIONS AND DATA P1 P2 P3 P4 P5 P6 P7 EFL 7.264 −12.117 35.980 81.979 −145.198 729.922 2100.036 F/No. −1.450 −1.450 −1.450 −1.450 −1.450 9.400 −14.100 S10 3.154 50.878 −126.861 −163.460 −167.963 −167.403 168.654 S17 271.009 213.056 −113.646 61.255 −10.607 68.828 3.277 S24 2.350 −12.345 35.982 51.876 97.922 40.276 −104.616 S47 4.632 5.482 4.658 5.264 6.015 53.226 73.878 S53 −105.364 −104.868 −105.482 −104.798 −103.775 −14.725 2.050 S56 −1.550 −1.550 −1.550 −1.550 −1.550 43.752 35.462 S66 4.969 4.799 4.853 4.815 5.202 4.818 5.114

The prescription of binary surface 3 is included following the lens system optical prescription table listed above. The binary surface 3 adds phase to the wavefront. By providing binary surface 3, the second through fifth lens elements 2, 3, 4 and 5 in the focus portion of the lens can be made from relatively inexpensive glass, such as BK7, rather than expensive optical glass having abnormal dispersion characteristics, such as SFPL 51. While it is advantageous to include this binary surface 3 near the front of the lens system where the axial beam diameters are largest, it will readily appear to those skilled in the art that the binary (diffractive) surface may be provided elsewhere and that more than one such surface may be provided. Other methods of aberration correction may also be used advantageously. It should be noted that this embodiment also incorporates two aspheric surfaces 12 and 26.

FIG. 63 shows the zoom lens system with the zoom groups positioned at the longest focal length and the focus group focused at infinity. Similarly, the ray aberration graphs of FIG. 64 are at infinity focus and maximum focal length. It should be noted that the use of a binary surface in this embodiment is a modification that may be used in any of the embodiments of the invention disclosed herein or future variations of the invention.

FIGS. 65 and 66 illustrate an example of another embodiment of the present invention. This embodiment of the zoom lens system of the present invention is very similar to the embodiment of FIGS. 10-62, except that a binary (diffractive) surface is provided. Specifically, the binary surface is provided on the front surface (surface No. 6 in the prescription) of the third lens element from the left. As described above with respect to FIGS. 10-62, that third lens element is the first (front) of two lens elements comprising the second focus group FG2, which is movable axially for accomplishing the focusing together with the movable first focus group FG1 comprised of only the second lens element. The lens system optical prescription for the embodiment of FIGS. 65 and 66 is set forth below in the tables generally entitled “Tables for FIGS. 65 and 66.” TABLES FOR FIGS. 65 and 66 LENS SYSTEM OPTICAL PRESCRIPTION Glass Surface Radius Thickness Name OBJECT Infinity Variable S1 Infinity 50.000 S2 −617.930 5.200 S-LAM60 S3 425.207 Variable S4 −2291.780 4.900 S-TIH6 S5 545.459 Variable S6# 961.467 19.482 BK7 S7 −607.161 0.730 S8 1355.262 12.601 BK7 S9 −1118.653 Variable S10 986.310 20.386 S-FPL51 S11 −502.874 0.730 S12 343.826 21.232 S-FPL51 S13 64586.450 0.730 S14 181.736 24.150 S-FPLS3 SiS 476.848 Variable S16 208.678 3.120 S-LAH66 S17* 40.147 6.111 S18 67.136 3.150 S-LAH59 S19 56.870 14.527 S20 −98.690 2.730 S-LAH66 S21 90.992 12.506 S-TIH53 S22 −174.619 Variable S23 764.771 14.926 S-FPL52 S24 −66.842 0.400 S25 133.738 17.704 S-FPLS1 S26 −69.988 3.100 S-LAM66 S27 −1580.221 0.400 S28 65.214 9.613 S-N5L36 S29 129.561 Variable STOP Infinity 8.811 S31* −36.392 2.044 S-BSM14 S32 −425.016 6.131 S33 −43.308 5.233 S-TIHS3 S34 −33.861 0.200 S35 47.203 13.980 S-FPL51 S36 −41.565 2.400 S-LAM66 S37 −56.845 0.200 S38 −109.533 1.950 S-LAH63 S39 31.532 10.159 S-FPL51 S40 −173.403 45.721 S41 47.891 4.513 S-LAHS3 S42 −2514.287 41.843 S43 −23.807 9.483 S-LAH59 S44 −24.610 12.719 S45 61.223 3.114 S-FPL51 S46 −45.071 0.150 S47 24.918 3.242 S-BSM9 S48 −516.606 Variable S49 −72.073 1.059 S-LAL54 S50 23.513 2.783 S51 −18.951 0.900 S-LAH59 S52 −57.174 1.347 S53 −21.150 21.292 S-LAH6O S54 −31.181 Variable S55 −138.459 4.401 S-BAL22 S56 −75.648 0.300 S57 606.713 5.842 S-FPL51 S58 −96.488 0.300 559 113.288 7.382 S-FPLS1 560 −97.742 2.500 S-TIH6 S61 −366.723 0.300 S62 400.000 0.000 S63 38.760 8.585 S-FPL52 564 269.438 5.901 S65 115.000 0.450 S66 94.072 1.770 S-LAL54 S67 35.982 7.000 S68 −90.502 2.010 S-LAL8 S69 29.972 6.150 S-TIH53 S70 82.308 2.725 S71 79.000 9.670 S72 76.232 6.100 S-PHM52 S73 −75.003 0.761 S74 45.420 7.170 S-FSLS S75 −45.317 1.500 5-TIH53 S76 348.342 18.544 S77 Infinity 13.200 S-BSL7 S78 Infinity 2.000 S79 Infinity 33.000 BAFS2 S80 Infinity 0.000 S81 Infinity 0.000 IMAGE Infinity Note: Maximum image diameter = 11.3 mm *Surface profiles of aspheric surfaces S17 and S31 are governed by the following conventional equation: $Z = {\frac{({CURV})Y^{2}}{1 + \left( {1 - {\left( {1 + K} \right)({CURV})^{2}Y^{2}}} \right)^{1/2}} + {(A)Y^{4}} + {B(Y)}^{6} + {(C)Y^{8}} + {(D)Y^{10}}}$ where: CURV = 1/(Radius of Surface) Y = Aperture height, measured perpendicular to optical axis K, A, B, C, D = Coefficients Z = Position of surface profile for a given Y value, as measured along the optical axis from the pole (i.e. axial vertex) of the surface. The coefficients for The coefficients for the surface S17 are: the surface S31 are: K = −0.3564029 K = 0.4304792 A = −8.6827410e−007 A = 9.5769727e−007 B = −2.1510889e−010 B = 1.3131850e−009 C = −6.3664850e−014 C = −1.4559220e−012 D = −3.8937870e−018 D = 3.1953640e−015 # Surface profile of binary surface S6 is governed by the following conventional equation: Added Phase =A₁p² + A₂p⁴ + A₃p⁶ + A₄p⁸ + A₅p¹⁰ where: A₁, A₂, A₃, A₄ and A₅ are coefficients and p is the normalized radial coordinate at the surface. The normalizing factor is set at unity and the p's become simply radial coordinates. A1 = −0.038094023 A2 = −2.7327913e−006 A3 = 5.0795942e−010 A4 = −5.0245151e−014 A5 = 1.5103625e−018 VARIABLE THICKNESS POSITIONS AND DATA P1 P2 P3 P4 P5 P6 P7 EFL 7.428 12.285 19.009 32.781 65.564 93.100 144.823 F/No. 1.949 1.949 1.949 1.949 1.949 2.010 2.090 S0 Infinity 5322.630 2499.896 Infinity 5322.630 Infinity 5322.630 S3 18.151 48.521 79.959 18.151 48.521 18.151 48.521 S5 6.399 10.135 15.000 6.399 10.135 6.399 10.135 S9 71.409 37.303 1.000 71.409 37.303 71.409 37.303 S15 1.350 67.051 110.745 155.094 189.151 203.856 210.392 S22 319.660 247.857 197.854 142.790 92.653 65.474 50.046 S29 9.625 15.727 22.036 32.751 48.830 61.304 70.197 S48 1.498 1.498 1.498 1.498 1.498 2.823 4.711 S54 63.257 63.257 63.257 63.257 63.257 61.933 60.044 VARIABLE THICKNESS POSITIONS AND DATA P8 P9 P10 P11 P12 P13 EFL 206.030 486.383 715.335 2050.042 4776.501 1890.393 F/No. 2.360 2.840 5.600 14.500 14.500 5.600 S0 Infinity 5322.630 Infinity Infinity 8708.002 5322.630 S3 18.151 48.521 18.151 18.151 37.472 48.521 S5 6.399 10.135 6.399 6.399 8.770 10.135 S9 71.409 37.303 71.409 71.409 49.718 37.303 S15 215.814 218.878 223.339 224.980 224.980 223.339 S22 33.074 24.338 10.235 1.719 1.719 10.235 S29 81.746 87.419 97.063 103.934 103.934 97.063 S48 9.572 14.559 31.080 63.536 63.536 31.080 S54 55.183 50.196 33.675 1.220 1.220 33.675

The prescription of binary surface 6 is included following the lens system optical prescription table listed above. The addition of binary surface 6 to the basic lens system optical prescription of the embodiment of FIGS. 10-62 allows the substitution of less expensive glass, such as BK7, for the fluor-crown glass of lens elements 3 and 4 (third and fourth from the left in FIG. 65). Although other small changes are also made in the prescription, the zoom lens system of FIGS. 65 and 66 has the same number of lens elements and the same number of moving groups for focusing and zoom as the embodiment of FIGS. 10-62. FIG. 65 shows the zoom lens system with the zoom groups positioned at the longest focal length and the focus groups focused at infinity. Similarly, the ray aberration graphs of FIG. 66 are at infinity focus and the longest focal length.

FIGS. 67-70 illustrate an example of another embodiment of the present invention. This embodiment of the zoom lens system of the present invention has a zoom ratio of about 400:1. Specifically, this embodiment has a zoom range of focal lengths of about 7.47 mm (the position shown in FIG. 67) to about 2983 mm (the position shown in FIG. 68). As with the embodiment of FIGS. 10-62, this embodiment has three moving zoom lens groups ZG1, ZG2 and ZG3, with two of them in the front zoom lens portion and one in the rear zoom lens portion. The ray aberration graphs of FIGS. 69 and 70 are at paraxial effective focal lengths (EFL) of 7.47 mm and 2983 mm, respectively, and illustrate that this embodiment performs well, considering the extremely wide range of focal lengths and large zoom ratio which is similar to the performance characteristics of the embodiment of FIGS. 10-62. The optical diagrams of FIGS. 67 and 68 and the ray aberration graphs of FIGS. 69 and 70 are shown at infinity focus.

The lens system optical prescription of FIGS. 67-70 is set forth below in the tables generally entitled “Tables for FIGS. 67 thru 70.” The following data in the lens system optical prescription is set forth in the same manner and the legends have the same meanings as in the preceding lens system optical prescriptions. TABLES FOR FIGS. 67 thru 70 LENS SYSTEM OPTICAL PRESCRIPTION Glass Surface Radius Thickness Name OBJECT Infinity Variable S1 1018.780 15.000 LAH78 S2 277.432 28.775 S3 523.118 37.500 S-FPL51 S4 −634.022 1.500 S5 323.390 30.000 S-FPL51 S6# −2096.922 −0.001 S7* 177.503 27.000 S-FPL51 S8 667.737 Variable S9 363.133 6.000 TAF1 S10* 84.560 23.084 S11 −1731.870 4.500 TAF1 S12 117.736 21.933 S13 −68.241 4.672 TAF1 S14 1396.861 11.280 PBH71 S15 −123.171 Variable S16 −351.922 21.562 S-FPL51 S17 −87.960 0.750 S18 670.190 25.507 LAK21 S19 −96.809 4.500 FD6 S20 −253.794 18.318 S21 112.307 6.052 FCS S22 345.143 Variable STOP Infinity 6.066 S24* −49.612 4.500 PSK53A S25 45.951 6.491 FD15 S26 149.306 8.138 S27 −53.675 2.556 PSK53A S28 −436.714 15.264 FD8 S29 −53.001 30.067 S30 96.369 40.439 S-FPL51 S31 −47.937 4.500 S-LAH75 S32 −65.887 0.018 S33 314.723 4.500 S-LAH75 S34 44.980 33.625 S-FPL53 S35 −197.211 62.647 S36* 59.624 15.000 S-FPL53 S37 −45862.250 62.567 S38 Infinity 2.000 S39 −250.000 2.000 S-LAH66 S40 38.600 21.997 S41 −42.668 3.012 PBH23W S42 78.619 20.849 S-LAL8 S43 −54.572 0.250 S44 701.714 11.340 S-LAL8 S45 −96.232 0.250 S46 153.694 14.173 S-LAL8 S47 −120.652 0.250 S48 57.764 24.753 S-LAM2 S49 −654.450 3.706 P8H6W S50 36.175 17.533 S51 126.517 2.500 PBHS3W S52 123.911 5.000 S-BSM14 S53 −269.378 0.200 S54 119.317 5.000 S-BSM18 S55 249.395 Variable S56 77.473 2.500 S-LAH60 S57 24.795 8.736 S58 −17.880 2.000 S-LAH55 S59 −73.667 1.561 S60 −68.965 7.000 PBH53W S61 −23.620 0.200 S62 −39.257 2.000 S-LAH65 S63 −73.267 Variable S64* 40.900 24.089 S-BAL42 S65* −82.736 0.200 S66 68.814 3.000 PBH53W S67 33.834 Variable S68 47.963 12.055 S-BSL7 S69 −38.097 8.000 PBH6W S70 −61.203 Variable S71 Infinity 11.874 S-BSL7 S72 Infinity 14.000 IMAGE Infinity Note: Maximum image diameter = 11.0 mm *Surface profiles of aspheric surfaces S7, S10, S24, S36, S64 and S65 are governed by the following conventional equation $\begin{matrix} {Z = {\frac{({CURV})Y^{2}}{1 + \left( {1 - {\left( {1 + K} \right)({CURV})^{2}Y^{2}}} \right)^{1/2}} + {(A)Y^{4}} + {B(Y)}^{6} + {(C)Y^{8}} + {(D)Y^{10}} +}} \\ {(E)Y^{12}} \end{matrix}\quad$ where: CURV = 1/(Radius of Surface) Y = Aperture height, measured perpendicular to optical axis K, A, B, C, D, E = Coefficients Z = Position of surface profile for a given Y value, as measured along the optical axis from the pole (i.e. axial vertex) of the surface. The coefficients for The coeffidents for the surface S7 are: the surface S10 are: K = −0.01834396 K = 0.1385814 A = 4.6192051e−009 A = −6.1078514e−008 B = 2.9277175e−013 B = −1.7110958e−012 C = −5.3760139e−018 C = −1.4298682e−015 D = 4.4429222e−022 D = −7.3308393e−019 E = 0 E = 0 The coefficients for The coeffidents for the surface S24 are: the surface S36 are: K = −0.1283323 K = 0.009973727 A = −2.7157663e−007 A = 3.3999271e−008 B = 1.4568941e−010 B = 1.4717268e−010 C = −1.4055959e−012 C = −1.0665963e−013 D = 9.7130719e−016 D = 6.8463872e−017 E = 0 E = 0 The coefficients for The coeffidents for the surface S7 are: the surface S10 are: K = −4.594951 K = −0.2743554 A = 5.9382510e−006 A = 1.2036084e−006 B = −4.3333569e−009 B = 3.8383867e−009 C = −2.6412286e−013 C = −1.5101902e−011 D = 5.0607811e−015 D = 2.3291313e−014 E = −3.8443669e−018 E = −1.3549754e−017 # Surface profile of binary surface S6 is governed by the following conventional equation: Added Phase = A₁p² + A₂p⁴ + A₃p⁶ + A₄p⁸ + A₅p¹⁰ + A₆p¹² where: A₁, A₂, A₃, A₄, A₅ and A₆ are coeffidents and p is the normalized radial coordinate at the surface. The normalizing factor is set at unity and the p's become simply radial coordinates. A1 = −0.0183497 A2 = 0.1385814 A3 = −0.1283323 A4 = 0.0099737 A5 = −4.5949510 A6 = −0.2743554 VARIABLE THICKNESS POSITIONS AND DATA P1 P2 P3 P4 P5 P6 P7 EFL 7.471 11.746 18.475 29.059 45.676 649.701 2981.989 F/No. 1.600 1.600 1.600 1.600 1.600 6.000 18.000 S0 Infinity Infinity Infinity Infinity Infinity Infinity Infinity S8 3.884 47.335 81.309 107.642 127.477 147.901 156.198 S15 243.496 190.547 145.303 105.453 68.586 39.080 0.104 S22 5.292 14.777 26.064 39.600 56.513 65.772 96.339 S55 1.000 1.000 1.000 1.000 1.000 98.702 111.239 S63 117.540 117.540 117.540 117.540 117.540 30.129 0.368 S67 42.175 42.175 42.175 42.175 42.175 20.670 63.421 S70 14.512 14.512 14.512 14.512 14.512 25.727 0.199

Detailed Description of Folded Lens Embodiment. FIG. 71 is an optical diagram illustrating an example of still another embodiment of the present invention incorporating one or more mirrors for folding the lens for added compactness. The example of FIG. 71 is similar to the previously-described embodiments, with three general zoom groups identified as 50, 52 and 54. An intermediate image is located at 56. The focus group 66 is movable during focusing, but is stationary when the lens is at a constant focus. The aperture stop is located at 84. Unique to the folded zoom lens embodiment of FIG. 71 is a mirror 64 located between the front and rear zoom groups 52 and 54 for “folding” or bending the radiation rays. The embodiment of FIG. 71 may be employed in any camera, but is particularly suited for small cameras such as point-and-shoot handheld cameras because the folded design enables the lens to fit into a smaller space. FIG. 71 illustrates an SLR embodiment containing a reflex mirror 60 and an eyelens 62 for enabling a user to see the image while the reflex mirror 60 is in the position indicated in FIG. 71.

Embodiments of the present invention are particularly suited to folding because mirror 64 may be placed within the intermediate image space 58 in any area that does not interfere with the movement of the zoom groups 52 and 54. In contrast, conventional compact zoom lenses have lens elements that must retract into the body of the camera, which eliminates most or all or the air gaps within the lens and precludes the insertion of a mirror. In the example of FIG. 71, the mirror 64 is located on the image side of the intermediate image 56. However, in other embodiments, the mirror 64 may be located on the object side of the intermediate image 56. It should be understood that other embodiments of the present invention may have multiple folds (mirrors), and that the mirrors need hot be oriented at 45 degrees with respect to the optical axis.

The folded lens illustrated in the example of FIG. 71 enables several useful design possibilities and advantages. As mentioned above, the fold in the lens enables the zoom lens to take up less space. Furthermore, the folded zoom lens enables some or all of the lens elements to reside within the body of the camera, further improving compactness. In one embodiment, even the focus lens group 66 may reside entirely within the body of the camera, protecting the lens and making the camera even more compact. In addition, the folded zoom lens enables compact cameras to achieve a zoom ratio of about 10:1 or higher, compared to a maximum of about 4:1 in conventional compact cameras. Moreover, conventional SLR cameras require a bulky pentaprism for flipping the image, and thus compact cameras typically avoid through-the-lens viewing. However, because of the intermediate image 56 and mirrors 64 and 60 in the present invention, the final image is already properly oriented without the need for a bulky pentaprism, and through-the-lens viewing is made possible even in cameras of a compact size.

The exemplary folded zoom lens of FIG. 71 provides an EFL of about 12 mm to 120 mm, a zoom ratio of about 10:1, an “f” number range of about f/3 to f/5 at full aperture and a maximum field of view angle in object space of about 84.1 degrees to 10.3 degrees, and receives radiation within a waveband of at least 486 nm to 588 nm. The image generated by the embodiment of FIG. 71 is about 12 mm in height by about 18 mm in width with a diagonal dimension of about 21.65 mm, which is about half the size of the image in a conventional 35 mm still photography camera.

FIGS. 72A-72D are optical diagrams illustrating the folded zoom lens example embodiment of FIG. 71 at other zoom positions, with the folded lens shown in a flat (unfolded) orientation for clarity and the zoom groups in various exemplary positions. As in FIG. 71, the focus lens group 66 in the example of FIGS. 72A-72D is movable for focusing and stationary at a constant focus, and the mirror 64 and eyelens 62 are also stationary. The aperture stop is located at 84 and is movable during zooming. The zoom lens example of FIGS. 72A-72D is actually comprised of eight moving zoom groups 68, 70, 72, 74, 76, 78, 80 and 82, although it should be understood that other embodiments of the folded zoom lens may include more or fewer zoom groups. The folded zoom lens example of FIGS. 72A-72D utilizes all spherical surfaces, but it should be understood that other embodiments may employ aspheres and/or binary (diffractive) surfaces.

Detailed Description of Infrared Embodiment. FIGS. 73A-73C are optical diagrams for an example of an infrared (IR) embodiment of the zoom lens system of the present invention, illustrating various positions of the zoom groups. The intermediate image is located at 86. The focus group 88 is movable during focusing, but is stationary at a constant focus. The final image plane is located at 90, and the aperture stop is located at 92. The embodiment of FIGS. 73A-73C may be employed in low light and surveillance cameras because the zoom lens system is designed for infrared wavelengths. The example of FIGS. 73A-73C provides an EFL of 6.68 mm to 1201.2 mm, an “f” number range of f/2.00 to f/5.84, an image diagonal of 8.0 mm, a maximum field of view angle in object space of 64.5 degrees to 0.388 degrees, and a vertex length of 902.28 mm. There is a −4.93% distortion at the 6.68 mm focal length position and +0.34% distortion at the 1201.2 mm focal length position. This distortion increases the effective zoom ratio to 190:1. There are a total of nine elements in the example of FIGS. 73A-73C, with six elements (94, 96, 98, 100, 102 and 104) in the zoom kernel 106, and three elements (108, 110 and 112) in the zoom relay 114. Note that the “zoom kernel,” as referred to herein, represents all of the elements from object space to the intermediate image, while the “zoom relay,” as referred to herein, represents all of the elements from the intermediate image to the final image.

The lens system optical prescription for the IR embodiment of FIGS. 73A-73C is set forth below in the tables generally entitled “Tables for FIGS. 73A, 73B and 73C.” The following data in the lens system optical prescription is set forth in the same manner and the legends have the same meanings as in the preceding lens system optical prescriptions. TABLES FOR FIGS. 73A, 73B and 73C LENS SYSTEM OPTICAL PRESCRIPTION Refractive Surface Radius Thickness Material OBJECT Infinity Infinity S1 Infinity 25.000 S2* 341.091 15.000 GERMANIUM S3# 442.256 14.496 S4 628.089 15.000 ZNSE S5 817.176 Variable S6* 191.321 5.000 GERMANIUM S7 101.374 Variable S8 −108.986 5.000 GERMANIUM S9 −133.542 Variable S10* 132.195 10.000 GERMANIUM S11 215.451 106.451 S12* 44.406 7.000 GERMANIUM S13* 47.364 Variable S14* −146.583 5.000 GERMANIUM S15* −103.306 Variable S16* −48.015 6.000 ZNSE S17* −54.690 Variable S18* −134.510 5.000 GERMANIUM S19* −96.541 Variable STOP Infinity 74.251 IMAGE Infinity Note: Maximum image diameter = 8.0 mm *Surface profiles of aspheric surfaces S2, S6, S10, S12, S13, S14, S15, S16, S17, S18 and S19 are governed by the following conventional equation: $\begin{matrix} {Z = {\frac{({CURV})Y^{2}}{1 + \left( {1 - {\left( {1 + K} \right)({CURV})^{2}Y^{2}}} \right)^{1/2}} + {(A)Y^{4}} + {B(Y)}^{6} + {(C)Y^{8}} +}} \\ {{(D)Y^{10}} + {(E)Y^{12}} + {F(Y)}^{14} + {(G)Y^{16}}} \end{matrix}\quad$ where: CURV = 1/(Radius of Surface) Y = Aperture height, measured perpendicular to optical axis A, B, C, D, E, F, G = Coefficients Z = Position of surface profile for a given V value, as measured along the optical axis from the pole (i:e. axial vertex) of the surface. The coefficients for the The coefficients for the surface S2 are: surface S6 are: K = −0.3170663 K = 0.0000000 A = 7.1675212e−010 A = 8.8834511e−009 B = 4.6490286e−015 B = −1.1017434e−012 C = 3.1509558e−020 C = 4.2407818e−016 D = −3.0230207e−026 D = −4.5843672e−020 E = 1.8711604e−043 E = 0 F = 7.2023035e−034 F = 0 G = −1.6899714e−038 G = 0 The coefficients for the The coefficients for the surface S10 are: surface S12 are: K = 0.0000000 K = 0.1424633 A = −4.1468720e−008 A = −1.3741884e−008 B = −1.1864804e−012 B = 2.0574529e−010 C = 1.0375271e−016 C = 2.2356569e−013 D = 1.4819552e−020 D = −9.2592205e−016 E = 0 E = 0 F = 0 F = 0 G = 0 G = 0 The coefficients for the The coefficients for the surface S13 are: surface S14 are: K = 0.1341907 K = 0.0000000 A = 2.5853953e−007 A = −2.3627230e−006 B = 6.3040925e−010 B = −3.2069853e−009 C = −8.9182471e−013 C = 1.9995538e−012 D = −2.1087914e−016 D = −4.1873811e−015 E = 0 E = −4.5598387e−018 F = 0 F = 1.5355757e−021 G = 0 G = 2.7742963e−025 The coefficients for the The coefficients for the surface S15 are: surface S16 are: K = 0.0000000 K = 0.0000000 A = −1.9992749e−006 A = −5.5264489e−007 B = −2.7451965e−009 B = −3.4855834e−011 C = 2.5915567e−012 C = −1.5605019e−013 D = −5.4747396e−015 D = 8.4346229e−016 E = 1.0432409e−018 E = −2.6930213e−019 F = −9.7041838e−023 F = 7.0886850e−022 G = 3.5844261e−025 G = −4.8763355e−025 The coefficients for the The coefficients for the surface S17 are: surface S18 are: K = 0.0000000 K = 0.0000000 A = −1.9256081e−007 A = 4.5197079e−007 B = 9.7560057e−012 B = −4.7688707e−010 C = −3.1406997e−013 C = −2.2771179e−013 D = −4.6996712e−016 D = −7.3812375e−016 E = 4.3471337e−019 E = 6.1621050e−019 F = −3.7957715e−022 F = −2.9782920e−023 G = −2.4875152e−026 G = −2.8295343e−026 The coefficients for the surface S19 are: K = 0.0000000 A = 3.9066750e−007 B = −2.6768710e−010 C = −3.7378469e−013 D = −4.0450877e−016 E = 3.9230103e−019 F = −3.7514135e−023 G = −8.0738327e−027 # Surface profile of binary surface S3 is governed by the following conventional equation: Added Phase = A₁p² + A₂p⁴ + A₃p⁶ + A₄p⁸ + A₅p¹⁰ where: A₁, A₂, A₃, A₄ and A₅ are coefficients and p is the normalized radial coordinate at the surface. The normalizing factor is set at unity and the p's become simply radial coordinates. A1 = −0.0085882326 A2 = −1.2587653e−008 A3 = −5.4668365e−013 A4 = 8.4183658e−018 A5 = 1.3774055e−022 VARIABLE THICKNESS POSITIONS AND DATA P1 P2 P3 P4 P5 P6 EFL 6.677 7.583 9.331 11.805 14.069 23.805 F/No. 2.000 2.000 2.000 2.000 2.000 2.000 S5 5.000 25.000 55.000 85.000 105.000 155.000 S7 239.848 216.543 180.384 143.845 119.259 58.715 S9 72.916 76.220 82.379 88.919 93.S04 104.048 S13 276.674 276.674 276.674 276.674 276.674 276.674 S15 5.030 5.030 5.030 5.030 5.030 5.030 S17 29.517 29.517 29.517 29.S17 29.517 29.517 S19 5.000 5.000 5.000 5.000 5.000 5.000 VARIABLE THICKNESS POSITIONS AND DATA P7 P8 P9 P10 P11 P12 EFL 48.419 84.275 133.455 175.637 231.172 304.215 F/No. 2.000 2.000 2.000 2.300 2.900 3.400 S5 205.000 231.305 243.545 243.545 243.545 243.545 S7 16.543 30.757 72.218 72.218 72.218 72.218 S9 96.221 55.701 2.000 2.000 2.000 2.000 S13 276.674 276.674 276.674 248.444 220.313 187.659 S15 5.030 5.030 5.030 42.180 79.972 109.931 S17 29.517 29.517 29.517 22.953 12.626 5.000 S19 5.000 5.000 5.000 2.644 3.310 13.631 VARIABLE THICKNESS POSITIONS AND DATA P13 P14 P15 P16 P17 EFL 400.368 526.915 693.449 912.675 1201.182 F/No. 3.500 3.800 4.600 5.300 5.840 S5 243.545 243.545 243.545 243.545 243.545 S7 72.218 72.218 72.218 72.218 72.218 S9 2.000 2.000 2.000 2.000 2.000 S13 146.432 112.380 97.552 94.304 95.940 S15 114.831 95.642 67.311 40.305 16.014 S17 10.137 19.763 26.212 25.615 18.454 S19 44.821 88.436 125.146 155.997 185.814

FIGS. 74-76 are ray aberration graphs corresponding to the position of the zoom groups shown in FIGS. 73A-73C, respectively. The ray aberration graphs of FIGS. 74-76 are at paraxial effective focal lengths (EFL) of 6.68 mm, 133.46 mm, and 1201.18 mm, respectively, and a wavelength range of 8-12 microns. The optical diagrams of FIGS. 73A-73C and the ray aberration graphs of FIGS. 74-76 are shown at infinity focus.

Detailed Description of 3-5 micron Infrared Embodiment. FIG. 77 illustrates an unfolded layout of a second exemplary IR embodiment of the zoom lens system with lens elements and surfaces identified. Referring to FIG. 77, each lens element is identified by a numeral from 120 through 138 (by twos) and the general configuration of each lens element is depicted, but the actual radius of each lens surface is set forth below in the table entitled “TABLE FOR FIGS. 77 AND 78A-78F.” The lens surfaces are identified by the letter “S” followed by a numeral from S0 through S23. The optical axis is identified by the symbol “Ø”. Each lens element has its opposite surfaces identified by a separate but consecutive surface number as, for example, lens element 120 has lens surfaces S1 and S2, lens element 126 has lens surfaces S7 and S8 and so forth. The intermediate image is located between S10 and S12. An optical stop is located at S22. The real image surface is identified by the numeral S23. All of the lens surfaces are spherical except lens surfaces S2, S8, S9 and S21 which are aspheric surfaces that are non-spherical, non-plano but rotationally symmetrical about the optical axis.

There are a total of 10 elements in the example of FIG. 77, with five elements (120, 122, 124, 126 and 128) in the zoom kernel or first lens group 151, and five elements (130, 132, 134, 136 and 138) in the zoom relay or second lens group 156. The optical design of the second exemplary IR embodiment can be characterized as an NPP kernel followed by an NNP relay. Note that the “zoom kernel,” as referred to herein, represents all of the elements from object space to the intermediate image, while the “zoom relay,” as referred to herein, represents all of the elements from the intermediate image to the final image.

The light rays entering the zoom lens system at the left are comprised of exemplary axial field beams 160 and exemplary off-axis field beams 162, 164 and 166, with the outer light rays in each field beam referred to as rim rays and the inner light ray in each field beam referred to as a chief or principal light ray. The off-axis field beam whose rim ray is furthest from the optical axis is referred to as the off-axis field beam maximum rim ray. Note that the off-axis field beam chief ray first crosses the optical axis before the intermediate image, and later crosses the optical axis again at the optical stop.

Before describing the detailed characteristics of the lens elements, a broad description of the lens groups and their axial positions and movement will be given for the zoom lens system, generally designated 150, of this second exemplary embodiment of the present invention. Beginning from the end facing the object to be photographed, i.e. the left end in FIG. 77, the first lens group 151 comprises a first lens subgroup 152, a first zoom subgroup 153, a second zoom subgroup 154, and a third zoom subgroup 155. The first lens subgroup 152 is a positive-powered subgroup and comprises singlet lens element 120 which gathers light from object space. The first lens subgroup 152 is movable during focusing, but is stationary and at a fixed distance with respect to the image plane S23 at a constant focus. The first zoom subgroup 153 is a negative-powered subgroup and comprises singlet lens elements 122 and 124. The second zoom subgroup 154 is a positive-powered subgroup and comprises a singlet lens element 126. The third zoom subgroup 155 is a positive-powered subgroup and comprises a singlet lens element 128. A second lens group 156 comprises a fourth zoom subgroup 157, a fifth zoom subgroup 0.158, and a sixth zoom subgroup 159. The fourth zoom subgroup 157 is a negative-powered subgroup and comprises a singlet lens element 130. The fifth zoom subgroup 158 is a negative-powered subgroup and comprises a singlet lens element 132. The sixth zoom subgroup 159 is a positive-powered subgroup and comprises singlet lens elements 134, 136 and 138, and includes an optical stop at S22. Although element 138 in the sixth zoom subgroup is rather thin in the example provided, in alternative embodiments this element may be thickened to improve its manufacturability. An axially movable intermediate image is located between the third zoom subgroup 155 and the fourth zoom subgroup 157. The second exemplary IR embodiment of the zoom lens system is set forth below in the table entitled “TABLE FOR FIGS. 77 AND 78A-78F.”

There are six independently moving groups altogether, three on the object side and three on the image side of the intermediate image. The horizontal arrows with arrowheads on both ends in the upper portion of FIG. 77 indicate that each of the zoom subgroups 153-159 are movable in both axial directions along the optical axis, some in a monotonic manner (i.e. in only one direction when progressing from one extreme to the other of adjustments) and others in a non-monotonic manner. While only the lens elements are physically shown in FIG. 77, it is to be understood that conventional mechanical devices and mechanisms are provided for supporting the lens elements and for causing axial movement of the movable groups in a conventional lens housing or barrel.

Note that the space between lens elements as shown in FIG. 77 and FIGS. 78A-78F suggests that a fold mirror could be located between zoom subgroups 154 and 155 and/or between the optical stop at S22 and the final image at S23 to create a folded embodiment.

The embodiment of FIG. 77 may be employed in low light and surveillance cameras because the zoom lens system is designed for IR wavelengths. The example of FIG. 77 provides an EFL of about 11.8 mm to 1137.1 mm, an “f” number range of about f/2.80 to f/4.00, an image diagonal of about 18.0 mm, a maximum field of view angle in object space of about 0.45 degrees to 37.36 degrees, and a vertex length from the front vertex (i.e. surface S1) to the final image (i.e. surface S22) of about 945 mm. There is a 1.55% distortion at the 11.8 mm focal length position and 2.14% distortion at the 1137.1 mm focal length position. This distortion increases the effective zoom ratio to approach about 100:1.

FIGS. 78A-78F are optical diagrams for the second exemplary IR embodiment of the zoom lens system, illustrating various positions of the zoom groups. It should be noted that lens elements 120 and 122 (the leftmost two elements) in FIG. 78A, although apparently touching, are in fact separated by a gap. Note also that in FIG. 78F, all rim rays for both the axial field beam and the off-axis field beams are roughly superimposed on each other, which enables the front lens element 120 to be made smaller and cheaper. In particular, the off-axis field beam maximum rim ray height (distance from rim ray to optical axis) is about 158.82 mm, and the axial field beam rim ray height is about 149.53 mm. The ratio of the off-axis field beam maximum rim ray distance to the axial field beam rim ray distance is about 1.062, which indicates that the first lens subgroup elements had to be made larger than ideal by only about 6.2%. It should be understood that a ratio of less than 1.25 is generally acceptable. Ideally, the off-axis field beam maximum rim rays and the axial field beam rim rays would be exactly superimposed on each other, resulting in a ratio of 1.000 and optimal size and cost for at least the first lens group.

The lens system optical prescription and fabrication data for the second exemplary IR embodiment of FIGS. 77 and 78A-78F is set forth below in the table generally entitled “TABLE FOR FIGS. 77 AND 78A-78F.” In the TABLE FOR FIGS. 78A-78F, the first column “ITEM” identifies each optical element, with the same numeral or label as used in FIG. 77. The second and third columns identify the “Group” and “Subgroup,” respectively, to which that optical element (lens) belongs with the same numerals used in FIG. 77. The fourth column “Surface” is a list of the surface numbers, of the object S0, the Stop (iris) S22, the image plane S23 and each of the actual surfaces of the lenses, as identified in FIG. 77. The fifth column “Zoom Position” identifies six typical zoom positions (Z1-Z6) of the zoom subgroups 153-159 (illustrated in FIGS. 78A-78F) wherein there are changes in the distance (separation) between some of the surfaces listed in the fourth column, as described below more thoroughly. The sixth column, headed by the legend “Radius of Curvature,” is a list of the optical surface radius of curvature for each surface, with a minus sign (−) meaning the center of the radius of curvature is to the left of the surface, as viewed in FIG. 77, and “Infinity” meaning an optically flat surface. The asterisk (*) for surfaces S2, S8, S9 and S21 indicate these are aspheric surfaces for which the “radius of curvature” is a base radius, and the formula and coefficients for those two surfaces are set forth as a footnote to the TABLE FOR FIGS. 77 AND 78A-78F at the * (asterisk). The seventh column “Thickness or Separation” is the axial distance between that surface (fourth column) and the next surface. For example, the distance between surface S3 and surface S4 is 9.0 mm.

The eighth column of the TABLE FOR FIGS. 77 AND 78A-78F provide the refractive material of each lens element. The last column of the TABLE FOR FIGS. 77 AND 78A-78F headed “Aperture Diameter” provides the maximum diameter for each surface through which the light rays pass. All of the maximum aperture diameters, except for the Stop surface S22, are calculated assuming an image diagonal of 18 mm and a relative aperture ranging from f/2.8 at the shortest focal length to f/4.0 at the longest focal length. The maximum aperture diameters of the Stop surface S22 for Zoom Positions Z1-Z6 are 30.170 mm, 29.727 mm, 28.999 mm, 28.286 mm, 25.654 mm and 21.076 mm, respectively. The maximum relative apertures (f-number) for Zoom Positions Z1-Z6 are f/2.80, f/2.86, f/2.93, f/3.00, f/3.30 and f/4.00, respectively. Depending on the choice of the value of the maximum relative apertures for Zoom Positions Z1-Z6, then in one or more zoom positions a very small negative air gap may occur at the edges of certain elements between zoom subgroups. Those skilled in the art will realize that the small negative air gap can be removed from the system by routine optimization without changing the basic design. TABLE FOR FIGS. 77 AND 78A-78F OPTICAL PRESCRIPTION Radius of Thickness or Aperture Sub- Zoom Curvature Separation Refractive Diameter Item Group Group Surface Position (mm) (mm) Material (mm) S0 (Object) Infinity 25.00 120 151 152 S1 All 215.343 28.544 Silicon 317.642 S2 Z1 269.106* 9.864 308.262 Z2 57.468 Z3 108.517 Z4 117.957 Z5 132.937 Z6 135.615 122 151 153 S3 All 637.888 9.000 Germanium 187.169 S4 All 247.226 11.642 174.123 124 151 153 S5 All 228.929 8.000 Silicon 166.617 S6 Z1 161.278 244.587 157.148 Z2 220.842 Z3 150.487 Z4 74.335 Z5 22.911 Z6 11.974 126 151 154 S7 All 288.682 15.448 Silicon 176.490 S8 Z1 1321.765* 212.856 174.473 Z2 233.828 Z3 270.854 Z4 362.883 Z5 443.606 Z6 460.309 128 151 155 59 All 83.756* 11.053 Silicon 105.651 S10 Z1 159.357 160.888 103.666 Z2 115.791 Z3 97.933 Z4 72.886 ZS 28.278 Z6 20.171 S11 (dummy) Z1 Infinity 74.210 Z2 46.803 Z3 3.191 Z4 3.253 Z5 57.219 Z6 19.714 130 156 157 S12 All −32.997 12.500 Silicon 29.867 S13 Z1 −45.308 1.830 36.698 Z2 29.317 Z3 74.625 Z4 73.197 Z5 0.800 Z6 1.897 132 156 158 S14 All −28.877 10.206 Germanium 23.882 S15 Z1 −44.286 1.917 30.694 Z2 0.995 Z3 0.100 Z4 0.926 Z5 4.846 Z6 18.907 134 156 159 S16 All 6208.244 13.998 Germanium 37.741 S17 All 264.338 0.400 40.076 136 S18 All 171.855 11.452 Silicon 41.269 S19 All −84.226 0.400 42.354 138 S20 All −128.685 1.000 Silicon 41.072 S21 Z1 −156.416* 1.254 41.075 Z2 1.696 Z3 0.750 Z4 1.699 Z5 15.734 Z6 38.441 S22 (Stop) All Infinity 79.221 S23 (Image) All Infinity 0.000 *Surface profiles of aspheric surfaces S2, S8, S9 and S21 are governed by the following conventional equation: $\begin{matrix} {Z = {\frac{({CURV})Y^{2}}{1 + \left( {1 - {\left( {1 + K} \right)({CURV})^{2}Y^{2}}} \right)^{1/2}} + {(A)Y^{4}} + {B(Y)}^{6} + {(C)Y^{8}} +}} \\ {{(D)Y^{10}} + {(E)Y^{12}} + {F(Y)}^{14}} \end{matrix}\quad$ where: CURV = 1/(Radius of Curvature) Y = Aperture height, measured perpendicular to optical axis K, A, B, C, D, E, F = Coefficients Z = Position of surface profile for a given Y value, as measured along the optical axis from the pole (i.e. axial vertex) of the surface. The coefficients for the surface S2 of item 1 are: K = −0.23909 A = −1.20061E−09 B = 7.10421E−15 C = −6.54538E−21 D = 1.74055E−26 E = 2.64213E−29 F = −1.38143E−33 The coefficients for the surface S8 of item 4 are: K = 28.74452 A = 1.70772E−09 B = 6.46357E−14 C = −6.99028E−18 D = 2.65455E−21 E = −4.37148E−25 F = 2.27757E−29 The coefficients for the surface S9 of item 5 are: K = −0.321348 A = −1.84849E−07 B = −3.24508E−11 C = 4.30816E−14 D = −2.13370E−18 E = −7.80714E−21 F = 1.67339E−24 The coefficients for the surface S21 of item 10 are: K = 1.125040 A = 8.42238E−07 B = 2.42138E−11 C = 4.68290E−13 D = 1.19515E−15 E = −2.58757E−18 F = 3.72479E−21

The foregoing footnote * to the TABLE FOR FIGS. 77 AND 78A-78F includes the equation for calculating the shape of the aspheric surfaces S2, S8, S9 and S21 for the value Z, wherein CURV is the curvature at the pole of the surface, Y is the height or distance from the optical axis of a specific point on the surface of the glass, K is the conic coefficient, and A, B, C, D, E and F are the 4th, 6th, 8th, 10th, 12th and 14th, respectively, order deformation coefficients. As noted above, for illustrating the scope and versatility of the present invention there are six different Zoom Positions Z1-Z6 set forth in the data of the TABLE FOR FIGS. 77 AND 78A-78F which provide specific data for six different positions for the six movable zoom subgroups. The Zoom Positions Z1-Z6 are representative of six positions of the zoom subgroups 153-159 with Zoom Positions Z1 and Z6 being the extreme positions and Z2, Z3, Z4 and Z5 being intermediate positions. Of course, it will be understood that continuous zooming is available between the extreme Zoom Positions Z1 and Z6, and that any combination of continuous zooming is available within the described zoom ranges with the lens system 150. In addition, continuous focusing is available over the full range of axial motion of the first lens group 152.

The Effective Focal Length (EFL), Full Field Of View (FFOV) and F-number of the lens system 150 varies for the different Zoom Positions. Referring again to FIGS. 78A-78F, the zoom lens system 150 is shown with the zoom groups in various Zoom Positions and with light ray traces for those positions. FIG. 78A represents the zoom position Z1 for which data is set forth above in the TABLE FOR FIGS. 77 AND 78A-78F with an EFL of about 11.787 mm, a FFOV of about 74.72°, and an F-number of about 2.8. FIG. 78B represents the zoom position Z2 from the TABLE FOR FIGS. 77 AND 78A-78F with an EFL of about 22.999 mm, a FFOV of about 42.74°, and an F-number of about 2.9. FIG. 78C represents the zoom position Z3 from the TABLE FOR FIGS. 77 AND 78A-78F with an EFL of about 54.974 mm, a FFOV of about 18.6°, and an F-number of about 2.9. FIG. 78D represents the zoom position Z4 from the TABLE FOR FIGS. 77 AND 78A-78F with an EFL of about 125.359 mm, a FFOV of about 8.22°, and an F-number of about 3.0. FIG. 78E represents the zoom position Z5 from the TABLE FOR FIGS. 77 AND 78A-78F with an EFL of about 359.536 mm, a FFOV of about 2.86°, and an F-number of about 3.3. FIG. 78F represents the zoom position Z6 from the TABLE FOR FIGS. 77 AND 78A-78F with an EFL of about 1137.054 mm, a FFOV of about 0.9°, and an F-number of about 4.0.

From the specifications for the individual lens elements (items 120-138 by twos) and the separation between lens elements set forth in the TABLE FOR FIGS. 77 AND 78A-78F, the focal lengths of each lens element and then each group of lens elements (i.e. first lens group 152, first zoom subgroup 153, second zoom subgroup 154, third zoom subgroup 155, fourth zoom subgroup 157, fifth zoom subgroup 158, and sixth zoom subgroup 159) may be calculated by using CODE V® optical design software that is commercially available from Optical Research Associates, Inc., Pasadena, Calif., U.S.A., at a temperature of 20° C. (68° F.) and standard atmospheric pressure (760 mm Hg), and those calculated group focal lengths are as follows:

-   -   First lens subgroup 152 (element 120)=322.994 mm;     -   First zoom subgroup 153 (elements 122 and 124)=−88.338 mm;     -   Second zoom subgroup 154 (element 126)=150.688 mm;     -   Third zoom subgroup 155 (element 128)=65.962 mm; and     -   Fourth zoom subgroup 157 (element 130)=−178.124 mm.     -   Fifth zoom subgroup 158 (element 132)=−54.620 mm.     -   Sixth zoom subgroup 159 (elements 134, 136 and 138)=35.153 mm.

As mentioned above, the zoom lens system 150 is provided with one optical stop at the surface S22 which controls the diameter of the aperture through which light rays may pass at that point to thereby cause any light rays in the zoom lens system radially beyond that diameter to be stopped. The optical stop is the location at which a physical iris is located. The iris is located within or at an end of the sixth zoom subgroup 159, and moves with that zoom subgroup. Note that in FIG. 78A, for example, the rim rays pass through S22 with room to spare, while in FIG. 78F, the rim rays are almost touching the extreme edges of S22 as they pass through the optical stop. This shows that the iris located at S22 must open as the focal length increases. To maintain a constant f-number at the image, the iris must “zoom” or change. In other words, the iris must be adjusted for constant aperture. A separate cam may be used to open or close the iris during zooming. In addition, it should be noted that all of the lens element surface apertures, set forth in the TABLE FOR FIGS. 77 AND 78A-78F, act as field stops at all focus and zoom positions as depicted in FIGS. 78A-78F. The size of the aperture of iris S22 is adjusted as the sixth zoom subgroup 159 moves axially, as described above, with respect to the maximum aperture diameters listed in the TABLE FOR FIGS. 77 AND 78A-78F and is given with its largest value in the TABLE FOR FIGS. 77 AND 78A-78F.

In the second exemplary IR embodiment of the zoom lens system, the sensor located at the image plane S23 is responsive not to light but to the amount of heat given off by the objects being viewed, and captures differences in the heat given off by the objects down to a Minimum Resolvable Temperature Difference (MRTD). To do this, the sensor averages the temperature of elements in the scene being viewed. The sensor ideally should not “see” any lens structure, otherwise the temperature of the lens structure would be averaged into the scene and cause image errors. Therefore, in embodiments of the present invention, the stop (i.e. the iris located at the stop) is part of the detector, and the detector including the stop is cooled to reduce electronic noise, producing a “cold stop.”

The six zoom subgroups 153-159 are each axially movable independently and their respective movements are coordinated by any convenient means, such as conventional mechanical devices such as cams or the like, to accomplish the desired zooming function.

FIGS. 79A-79F illustrate the diffraction modulation transfer function (MTF) for the same light rays entering the lens system at the relative field heights shown in FIGS. 78A-78F according to embodiments of the present invention. In FIGS. 79A-79F, the x-axis represents the spatial frequency (resolution) in cycles per millimeter, and the y-axis represents a relative modulation value (an indication of image quality). The diffraction MTF curves of FIGS. 79A-79F are polychromatic, using the same wavelengths and X and Y field fans, but with wavelength weights. Note that at a spatial frequency of about 15 cycles/mm, at the extreme right distal end of each of the plots, the diffraction MTF for all of the field fans in each of the plots are clustered with a modulation range of about 0.65 to 0.82. In general, diffraction MTFs greater than 0.50 are desired, and a lens is said to be “diffraction limited” (ideal) if the diffraction MTFs are greater than 80%. Thus, there is not much of a dropoff from the diffraction limit in the lens of the present invention. The maximum distortion in the six zoom positions of FIGS. 79A-79F is about 3.5%.

Although the present invention has been fully described in connection with embodiments thereof with reference to the accompanying drawings, it is to be noted that various changes and modifications will become apparent to those skilled in the art. Such changes and modifications are to be understood as being included within the scope of the present invention as defined by the appended claims. 

1. An infrared zoom lens system for forming a final image of an object, said system having an object side and an image side and forming a first intermediate real image between the object and the final image, said system comprising: a first lens group including at least two lens elements and located between the object and the first intermediate real image, said first lens group comprising at least one zoom subgroup which is moved to change the size (magnification) of the first intermediate real image; a second lens group including at least two lens elements and located between the first intermediate real image and the final image, at least a portion of which is moved to change the size (magnification) of the final image; and an optical stop located between the intermediate image and the final image; wherein off-axis field beam chief rays first cross an optical axis of the infrared zoom lens system on the object side of the intermediate image and then cross the optical axis again at the optical stop; and wherein a ratio of a maximum off-axis field beam rim ray to an axial field beam rim ray at a lens surface of the first lens group adjacent to object space at a longest focal length of the zoom lens system is less than about 1.25.
 2. The infrared zoom lens system as recited in claim 1, wherein the optical stop is located between a last element surface of the second lens group and the final image.
 3. The infrared zoom lens system as recited in claim 1, wherein the infrared zoom lens system is capable of forming the final image from received radiation in the range of about 3-5 microns.
 4. The infrared zoom lens system as recited in claim 1, wherein the first lens group comprises five lens elements and the second lens group comprises five lens elements.
 5. The infrared zoom lens system as recited in claim 1, wherein the first lens group and the second lens group comprise a seven group system with one axially stationary lens subgroup and six axially movable zoom subgroups.
 6. The infrared zoom lens system as recited in claim 1, wherein the first lens group comprises three zoom subgroups and the second lens group comprises three zoom subgroups.
 7. The infrared zoom lens system as recited in claim 1, wherein the first lens group comprises one axially stationary lens subgroup.
 8. The infrared zoom lens system as recited in claim 1, wherein the lens elements include one or more germanium lens elements and one or more silicon lens elements.
 9. The infrared zoom lens system as recited in claim 1, wherein at least one of the lens elements includes an aspheric surface.
 10. The infrared zoom lens system as recited in claim 5, wherein the first lens group comprises a first lens subgroup of positive power, a first zoom subgroup of negative power, a second zoom subgroup of positive power, and a third zoom subgroup of positive power, and the second lens group comprises a fourth zoom subgroup of negative power, a fifth zoom subgroup of negative power, and a sixth zoom subgroup of positive power.
 11. An infrared zoom lens system for forming a final image of an object, said system having an object side and an image side and forming a first intermediate real image between the object and the final image, said system comprising: a first lens group including a first five lens elements and located between the object and the first intermediate real image, said first lens group comprising at least one zoom subgroup which is moved to change the size (magnification) of the first intermediate real image and having an optical design set forth in a table below where said first five lens elements are identified in an Item column as items 120, 122, 124, 126 and 128; a second lens group including a second five lens elements and located between the first intermediate real image and the final image, at least a portion of which is moved to change the size (magnification) of the final image, said second lens group having an optical design set forth in the table below where said second five lens elements are identified in the Item column as items 130, 132, 134, 136 and 138; and an optical stop located between the intermediate image and the final image; wherein a Surface column in the table identifies surfaces of items, Object in the Surface column is a location of an object on the object side, Stop in the Surface column is a location of the optical stop, Image in the Surface column is a location of the final image, a Radius of Curvature column in the table sets forth a radius of a corresponding surface, a Thickness or Separation column in the table sets forth a distance from one surface to a next surface, a Refractive Material column in the table identifies material between a corresponding surface and a next surface, and an Aperture Diameter column in the table sets forth a maximum diametric diameter of light rays passing through the corresponding surface; wherein off-axis field beam chief rays first cross an optical axis of the infrared zoom lens system on the object side of the intermediate image and then cross the optical axis again at the optical stop; and wherein a ratio of a maximum off-axis field beam rim ray to an axial field beam rim ray at a lens surface of the first lens group adjacent to object space at a longest focal length of the zoom lens system is less than about 1.25. Radius of Thickness or Aperture Sub- Zoom Curvature Separation Refractive Diameter Item Group Group Surface Position (mm) (mm) Material (mm) S0 (Object) Infinity 25.000 120 151 152 S1 All 215.343 28.544 Silicon 317.642 S2 Z1 269.106* 9.864 308.262 Z2 57.468 Z3 108.517 Z4 117.957 Z5 132.937 Z6 135.615 122 151 153 S3 All 637.888 9.000 Germanium 187.169 S4 All 247.226 11.642 174.123 124 151 153 S5 All 228.929 8.000 Silicon 166.617 S6 Z1 161.278 244.587 157.148 Z2 220.842 Z3 150.487 Z4 74.335 Z5 22.911 Z6 11.974 126 151 154 S7 All 288.682 15.448 Silicon 176.490 S8 Z1 1321.765* 212.856 174.473 Z2 233.828 Z3 270.854 Z4 362.883 Z5 443.606 Z6 460.309 128 151 155 S9 All 83.756* 11.053 Silicon 105.651 S10 Z1 159.357 160.888 103.666 Z2 115.791 Z3 97.933 Z4 72.886 Z5 28.278 Z6 20.171 S11 (dummy) Z1 Infinity 74.210 Z2 46.803 Z3 3.191 Z4 3.253 Z5 57.219 Z6 19.714 130 156 157 S12 All −32.997 12.500 Silicon 29.867 S13 Z1 −45.308 1.830 36.698 Z2 29.317 Z3 74.625 Z4 73.197 Z5 0.800 Z6 1.897 132 156 158 S14 All −28.877 10.206 Germanium 23.882 S15 Z1 −44.286 1.917 30.694 Z2 0.995 Z3 0.100 Z4 0.926 Z5 4.846 Z6 18.907 134 156 159 S16 All 6208.244 13.998 Germanium 37.741 S17 All 264.338 0.400 40.076 136 S18 All 171.855 11.452 Silicon 41.269 S19 All −84.226 0.400 42.354 138 S20 All −128.685 1.000 Silicon 41.072 S21 Z1 −156.416* 1.254 41.075 Z2 1.696 Z3 0.750 Z4 1.699 Z5 15.734 Z6 38.441 S22 (Stop) All Infinity 79.221 S23 (Image) All Infinity 0.000 